Command & Control
Autopilots & Payloads
Tracking & IFF
Transponders
Scoring Systems
Flight Termination &
Range Safety
Custom Test Sets
Fort Walton Beach, FL 32548 | 850-244-2332 | 1-888-325-9422 | www.gomicrosystems.com
PH: (850) 244-2332
Note to exporters: If this equipment is purchased for export, it will require an export license under
International Traffic in Arms Regulations (ITAR) approved by the U.S. Department of State. An end
user statement must be submitted to Micro Systems, Inc. with your purchase order for our review. The
end user statement must be on company letterhead with an authorized signature and is to be either
faxed or mailed (no e-mails). We will require that you supply our Contracts Department with a valid
export license number and expiration date before any equipment will be shipped.
Supporting The Defense Industry Since 1976
Micro Systems, Inc. is an AS9100C and ISO 9001:2008 certified
wholly owned subsidiary of Kratos Defense and Security
Solutions, headquartered in Fort Walton Beach Florida. Since
1976 we have been continuously exceeding our customers’
expectations in engineering, production and field services.
Our principal business is the design, development, and
manufacture of sophisticated systems used in a broad range of
advanced defense applications primarily in the unmanned systems
segment of the aerospace and defense industry. In our over 30
year history we have served the defense industry with a wide
range of solutions and products for Command and Control, Flight
Telemetry, Over-the-Horizon Communication, Electronic
Warfare, Flight Line Test, and Range Safety.
We offer a broad range of products including Unmanned Vehicle
Control Systems, Sophisticated Avionics, Radar Tracking and
Datalink Transponders, Scoring Systems, Custom Test
Equipment, and Advanced Flight Termination Systems.
This catalog contains just a few of the many products that we
offer to the industry. If you do not find a product that meets the
exact needs of your requirements please contact us and we can
discuss options to modify an existing product or design a new
product.
Our experienced team of management, engineering, and
production personnel are goal oriented, recognized leaders in the
defense industry. They follow through from design, prototype,
qualification, manufacturing, test to final delivery.
We are dedicated to providing total customer satisfaction and have
a team in-place with the resources, commitment, and Total
Quality mind-set necessary to provide high-performance, high
reliability products to the Aerospace and Defense Industry.
We are proud to serve you.
Our Vision
To be the premier global supplier of unmanned vehicle systems, software products, and engineering services to
continuously exceed our customer’s expectations by providing the highest degree of quality and customer service.
1
MICRO SYSTEMS, INC.
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Micro Systems is committed to achieving the
highest level of quality in every aspect of its
business practices.
Capabilities
Micro Systems maintains a staff of highly skilled and
experienced systems, hardware, and software engineers. We
can provide off the shelf or custom developed solutions from
individual circuit card assemblies through large integrated
systems. Our environmental experience ranges from ground
benign (air conditioned and heated buildings) to flightline to
airborne uninhabited fighter. Our products incorporate
analog/digital/mixed signal, RF to 6 GHz, high performance
embedded software, and graphical user interfaces.
Quality System
We maintain a comprehensive Quality Assurance Program
centered on the concepts of Total Quality. The program fully
complies with the requirements of AS9100C and ANSI/ISO/
ASQ Q9001-2008. The Quality Program consists of continuous
improvement activities involving everyone in the organization,
managers and workers, in a totally integrated effort to improve
performance at every level. This approach originates with the
President whose obsession with quality is constantly visible to
all employees.
Our quality system is independently reviewed by BSi
Management Systems every six months.
We have been
certified continuously since January 1999.
2
LOCATIONS
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Headquarters
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 3257
PH: (850) 244-2332
FAX: (850) 243-1378
Micro Systems – Bldg 2
Micro Systems, Inc.
65 Hill Ave
Fort Walton Beach, FL 3257
PH: (850) 244-2332
FAX: (850) 243-1378
3
REPRESENTATIVES
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Domestic Representatives
United States – RF Simulation Products
Precision Marketing Inc.
Joe Penna
Southeast Region
PH: (954) 752-1700
FAX: (954) 973-6335
United States – Full Product Line
AeroGear
Joel Webber
East U.S. Region
PH: (561) 753-4327
Email: joe.penna@precision-marketing.com
Web: www.aerogear.us
Email: joel.weber@aerogear.us
Web: www.precision-marketing.com
Please check our
website for the latest
representative contact
information
International Representatives
Germany – Full Product Line
TelData Systems
Herb Wutz
PH: +49-8121-410118
FAX: +49-8121-226692
Email: hwutz@teldatasystems.de
Web: www.teldatasystem.de
Korea – Full Product Line
Global Overseas Co., Ltd.
E.S. Yi & J.J. Song
PH: +82-02-338-7031
FAX: +82-02-338-1098
Email: globalko@hanafos.com
Web: www.globaladvanceinc.com
Italy – Full Product Line
Crisel
Eugenia Finocchiaro
PH: +39-06-35498681
FAX: +39-06-35498686
Email: finocchiaro@crisel.it
Web: www.crisel.it
Singapore, Malaysia, Brunei, &
Indonesia – Full Product Line
Precision Technologies Pte Ltd.
Richard Wong
PH: +65-6-273-4573
Email: richardw@pretech.com.sg
Web: www.pretech.com.sg
Thailand – Full Product Line
Thailand Siam Aviation Co., Ltd.
Warathan Makarabhirom
PH: +662-248-7360
FAX: +662-248-7634
Email: siamav@loxinfo.co.th
Turkey – Full Product Line
Photo-Sonics Intl Ltd
Bruce Hefford
PH: +44(0) 1844-260600
FAX: +44(0) 1844 260126
Taiwan – Full Product Line
Tai E Tradign Co. Ltd.
Frank Chu
PH: +886-2-2577-3325
FAX: +886-2-2577-9951
Email: frank.chu@taieco.com.tw
Web: www.taieco.com.tw
United Kingdom – Full Product Line
Photo-Sonics Intl Ltd
Bruce Hefford
PH: +44(0) 1844-260600
FAX: +44(0) 1844 260126
Email: bruce.hefford@photo-sonics.co.uk
Email: bruce.hefford@photo-sonics.co.uk
Web: www.photosonics.com
Web: www.photosonics.com
Australia – Full Product Line
Global Defense Solutions Pty Ltd.
Laurie Koster
PH: +61(0)2-4423-7959
Email: lkoster@globaldefence.com
Web: www.globaldefence.com
Korea (Us office) – Full Product Line
Global Advance, Inc.
W.C. Kim
PH: (818) 889-7054
FAX: (818) 889-3950
Email: globalwck@globaladvanceinc.com
Web: www.globaladvanceinc.com
Spain – Full Product Line
Industrializacion, S.A. (INSA)
Juan De Lorenzo
PH: +34(91) 5422005
FAX: +34(91)5424426
Email: juandelorenzo@industrializacion.es
4
PRODUCTS
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Unmanned Vehicle Control Systems p. 7
-- Ground Control Systems
Unmanned Vehicle Electronics
p. 15
-- Unmanned Vehicle Control Electronics
-- Command & Control Datalink Transponders
Radar Tracking Transponders
p. 49
-- 5, 20, 50 Watt C-Band
-- Ultra-Miniature
-- PC Programming Set
Scoring Systems
p. 55
-- AN/DSQ-50 Miss Distance Sensor
-- Scoring Ground Control Station
Test Sets
p. 61
-- C-Band Transponder Test Set
-- LRU Test Sets
-- Vehicle Checkout Test Sets
Flight Termination
-- Flight Termination Systems
-- Exciters and Receivers
-- Test Sets
5
p. 71
6
UNMANNED VEHICLE CONTROL SYSTEMS
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
The Micro Systems, Inc. Unmanned Vehicle Control Systems are developed based on our MOdular
Networked TArGet control Equipment (MONTAGE) architecture which offers the latest in performance,
flexibility, and cost effectiveness. These systems are available in Portable, Transportable, and Fixed Site,
configurations. Our Vehicle Control Systems can be configured to control up to eight air vehicles and/or a
mix of up to sixteen ground or sea surface vehicles, with a simultaneous mix of vehicle types and can be
field expanded with no change to system software (plug and play). Our systems have been interfaced to a
variety of remotely piloted vehicles including: BQM-167 (i and xi versions), Firejet, MQM-107 D/E, BQM74E, Chukkar, BQM-34 (-47 and -49), BQM-167A/I, BQM-167X, BQM-177A/I, Firejet, MSST, QUH-1 Rotary
Wing Target, QST-35 ship target, Falconet, and the High Speed Maneuverable Surface Target (HSMST).
7
8
UVCS
Data Sheet
AS9100C and ISO 9001:2008 Certified
Unmanned Vehicle Control System
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Multi-Vehicle Configuration
Features
Applications
Simultaneous Multi-vehicle control
Modular “Plug and Play” System
Interface to range infrastructure for
mission information sharing
Ruggedized Transportable System
Vehicle Independent Datalink
Air, Ground, and Marine Vehicle
Command and Control (C2)
Mission Planning
Simulation
Description
The Unmanned Vehicle Control System is a field proven C2 system based on the MONTAGE
architecture used to control remotely piloted vehicles or target drones. The system can control
multiple full and/or sub-scale fixed and rotary wing aerial targets and sea surface targets to a range of
200 nm line of site, or up to 330 nm with a minimum of 12dB of margin if using the optional relay
system, using differentially corrected GPS position data.
Our unique modular systems approach allows the system to be tailored to the customer’s specific
needs by purchasing only as much capability as required. Additional consoles and modules can be
easily added in the field. Vehicle command and telemetry configurations, telemetry displays, and
range maps can all be configured to the customer’s preferences.
The system operates independent of Data Link types and can accommodate multiple data links
and/or multiple frequencies simultaneously. The RF module can be connected directly via Ethernet,
or remotely to network through a router (e.g. T1, ISDN, microwave, etc.).
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
9
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Modular Systems Approach
Distributed Multi-processor System
Configurable using “Building Blocks – Purchase only as much capability as needed
Highly Cost Effective
High Capability Configurations Available
Vehicle and Datalink Independent
Configure with multiple datalinks simultaneously
High Capacity – for full scale vehicle
Reduced Capacity (reduced cost) – for subscale vehicles (MQM-107, BQM-167, Medium size UAV, UGV, USV)
Simultaneous Vehicle Operation – for multi-vehicle missions
Field Upgradeable
Additional consoles and modules can easily be added (up to 8 vehicles)
Temporary expansion for special mission requirements
Range Independent
No range specific functions for vehicle command and control
Range interface available for collecting/monitoring mission data
Highly Integrated Consoles and Open System Architecture
Fast and Easy Set-up (Typically less than 30 minutes)
Minimal inter-module connections
Choice of single or dual console Target Control Groups
TCP/IP interface between consoles and modules
Supports remote location of “Building Blocks” (location transparency)
Portable and Fixed Site system configurations are available
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
10
© 2010 Micro Systems, Inc
Specifications subject to change without notice
P-MONTAGE
Data Sheet
AS9100C and ISO 9001:2008 Certified
Portable Vehicle Control System
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Applications
Simultaneous Multi-vehicle control
Modular “Plug and Play” System
Interface to range infrastructure for
mission information sharing
Ruggedized Portable System
Vehicle Independent Datalink
Vehicle Command and Control (C2)
Mission Planning
Simulation
Description
The portable configuration of our Ground Control System (GCS) provides all of the capabilities of
our fixed and transportable control systems. The GCS can control multiple full and/or sub-scale fixed
and rotary wing targets and sea surface targets to a range of 200 nm line of site, or up to 330 nm with
a minimum of 12dB of margin if using the optional relay system, using differentially corrected GPS
position data.
Our unique modular systems approach allows the system to be tailored to the customer’s specific
needs by purchasing only as much capability as required. Additional consoles and modules can be
easily added in the field. Vehicle command and telemetry configurations, telemetry displays, and
range maps can all be configured to the customer’s preferences.
The system operates independent of Data Link types and can accommodate multiple data links
and/or multiple frequencies simultaneously. The RF module can be connected directly via Ethernet,
or remotely to network through a router (e.g. T1, ISDN, microwave, etc.).
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
11
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Modular Systems Approach
Distributed Multi-processor System
Configurable using “Building Blocks – Purchase only as much capability as needed
Highly Cost Effective
High Capability Configurations Available
Vehicle and Datalink Independent
Configure with multiple datalinks simultaneously
High Capacity – for full scale vehicle
Reduced Capacity (reduced cost) – for subscale vehicles (MQM-107, BQM-167, Medium size UAV, UGV, USV)
Simultaneous Vehicle Operation – for multi-vehicle missions
Field Upgradeable
Additional consoles and modules can easily be added (up to 8 vehicles)
Temporary expansion for special mission requirements
Range Independent
No range specific functions for vehicle command and control
Range interface available for collecting/monitoring mission data
Highly Integrated Consoles
Fast and Easy Set-up (Typically less than 30 minutes)
Minimal inter-module connections
Choice of single or dual console Target Control Groups
Ruggedized, Environmentally Protected Consoles
Ruggedized Laptops, keyboards, and command panels
Designed to meet MIL-STD-810 and MIL-STD-461 qualification
Open System Architecture
TCP/IP interface between consoles and modules
Supports remote location of “Building Blocks” (location transparency)
Common Console Design
Range Situation Displays (option) and System Control Consoles are physically and electrically identical
Fewer spares required
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
12
© 2010 Micro Systems, Inc
Specifications subject to change without notice
M-PAK
Data Sheet
AS9100C and ISO 9001:2008 Certified
Multi-Platform Appliqué Kit (M-PAK)
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Developed using proven technology
Modular design
Standard interfaces
Field upgradable
Ruggedized portable system
Vehicle Independent Datalink
Applications
Training
Weapons Evaluation
Tactical Operations
Route and Range Clearance
Equipment Transportation
Mining /Construction
Security/Perimeter Patrol
Commercial Use
Description
The Micro Systems Multi-Platform Appliqué Kit (M-PAK) is the next generation of Ground Vehicle
automation. The system can be used to quickly and easily convert your existing fleet of standard
human-driven vehicles into optionally-manned systems that can be driven in manned or unmanned
modes. M-PAK does NOT degraded ingress or egress characteristics for a driver when in manualdriving mode and has been designed from the ground up with safety as a top priority when in
automated modes of operation. It includes a roof-mount navigation module (NavModule), an
innovative quick-install steering actuator, actuators for acceleration and braking, transmission
controller, and an active safety system.
M-PAK is a scalable system that can be used as a stand-alone vehicle mobility kit or sensors can
be added to offer various levels of autonomy. It supports Tele-Op remote control operation using
Micro Systems fixed site and man-portable Command and Control (C2) systems, GPS waypoint
following, and Leader/Follower (manned/unmanned teaming). M-PAK allows for a semi-permanent
installation in a vehicle, which releases the user from committing to one vehicle platform or a
particular vehicle. It can move freely among a variety of vehicle types and enables optional
dependable unmanned capabilities for a number of applications.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
13
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Vehicle Installation Kit General Specifications
Quickly converts most human-driven vehicles into unmanned systems
Operates in Manual, Remote Control, GPS Path Following, and Leader/Follower Modes
Compatible with Micro Systems C2 Systems (fixed site and man-portable)
No driver ingress or egress interference
Includes Active Safety System
Designed with standardized components for easy upgrade and extended lifecycle
Multiple configurations available
Scalable to application
User Interfaces include: Ethernet, CAN/J1929, RS-232/422, and USB
Datalink Independent (UHF, WiFi, standard military datalinks)
Quick and easy installation
Power: 12VDC
Steering Actuation
NAVModule
Operator Control Unit
Actuators
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
14
© 2010 Micro Systems, Inc
Specifications subject to change without notice
UNMANNED VEHICLE ELECTRONICS
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Micro Systems, Inc. has designed and produced control electronics for high performance unmanned
aerial vehicles since 1976. In our over 30 years of continuous operation we have interfaced to virtually
every aerial target vehicle flown by the U.S. DoD. These vehicles are typically used as target drones,
and are capable of high performance maneuvers such as supersonic flight, barrel rolls, pitch-back, slice,
high G turns and weaves, and very low altitude operation. We have also interfaced to a variety of U.S.
Navy sea surface targets and U.S. Army ground targets. Based on our extensive and varied experience
we can design a control system for your unmanned vehicle needs.
15
16
UVMC
Data Sheet
AS9100C and ISO 9001:2008 Certified
Unmanned Vehicle Mission Computer
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Field Proven Hardware
Modular Design
High Performance Processing I/O
Ruggedized Aluminum Chassis
Qualified to MIL-STD-461E (EMI),
MIL-STD-810G (Env), MIL-HDBK781A (Reliability)
Hi-speed Mission Data Recording
Compatible RTOS’s: MQX, Linux,
Wind River, Green Hills
Applications
Vehicle Control System
Autopilot
Command and Telemetry
Vehicle Payload Interface
Remote Data Terminal
Description
The Unmanned Vehicle Mission Computer (UVMC) is a modular, high performance system that
provides maximum flexibility for easy integration into multiple platforms. It was developed with highlevel mission planning capabilities and vehicle sensor integration as key feature capabilities.
The field proven UVMC is designed with an advanced parallel processing architecture that
utilizes a 760 MIPS main processor for computationally intensive autopilot control algorithms and an
FPGA based processing module for Input/Output signal control requirements. This unique
architecture allows the core autopilot software to remain separate from the I/O software, thus
offloading I/O functions from the main processor.
The UVMC includes interfaces for external GPS and IMU modules as well as RS-232/485/422,
CAN, HDLC, 10Base100 Ethernet, JTAG, and ITCS. MIL-STD-1553B is also available as an optional
upgrade. A removable Compact Flash module is also available to support high speed data recording
requirements.
The UVMC utilizes a Common Interface Bus architecture that provides expansion capability for
additional I/O, a Inertial Navigation System (INS) module, and additional communication interfaces.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
17
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Characteristics
CPU Module:
Serial Interfaces:
Data Recording:
Standard I/O Module:
Discrete Outputs:
Discrete Inputs:
Proportional Inputs:
Freescale MPC5200B Main Processor (760 MIPS)
RS-232/485/422, CAN, HDLC, 10Base100 Ethernet, JTAG, ITCS, MIL-STD-1553 (optional)
Compact Flash
Xilinx Spartan 3A with MicroBlaze 32 bit processor (60 MIPS)
10 Type 1, 28VDC/Open, 1A | 8 Type 2, GND/Open, 500ma | Type 3 Open Collection
8 Type 1, 28VDC/Open | 6 Type 2, GND/Open | 4 Type 3, TTL
4 Type 1, 0 to +40VDC | 3 Type 2, 0 to +10VDC | 2 Type 3, -8mV to +54mV
Available Real Time Operating Systems (RTOS) and Board Support Packages
Compatible with: MQX, Linux, Wind River, Green Hills
Environmental (MIL-STD-810G) / EMI (MIL-STD-461E)
Temperature:
Cooling:
Vibration:
Altitude:
Shock:
Humidity:
EMI/RFI:
Operating: -40 C to +70 C
Passive Conductive (no moving parts)
Random, 0.4g2/Hz to 0.0429g2/Hz, 8 minutes per orthogonal axis
50,000 ft
Operating: 300G for 1ms, 3 pulses per axis
Up to 95% @ 40 C (all boards are conformal coated)
CE102, RE102, CS101, CS114, CS115 and RS103
Power Requirements
DC Power:
Consumption:
Protection:
22 to 32VDC (28VDC Nominal)
20 Watts max (standard unit)
Surge, Reverse, and Over Voltage protected
Physical
Size:
Weight:
Connectors:
Finish:
Installation:
5.00" W x 3.50" T x 7.25" D
6 pounds
44 and 62 pin D-Sub connectors, RJ45 connector, Compact Flash Interface
Powder Coat
Flange Mount Base Plate
Available Options
I/O Expansion Module with additional Input and Output Signal Capability
Inertial Navigation Module that includes a MEMS IMU and GPS Module
High Capacity Compact Flash Module
MIL-STD-1553B Interface
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
18
© 2010 Micro Systems, Inc
Specifications subject to change without notice
MSDL
Data Sheet
AS9100C and ISO 9001:2008 Certified
Multi-Service Data Link (MSDL) Transponder
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Field Proven Hardware
Modular Design
99 Available Frequency Channels in
the range of 359.5 MHz to 375 MHz
GMSK Modulation
Up to 35 watts RF Output Power
3 antenna ports
Ruggedized Aluminum Chassis
Applications
Autopilot Interface
Command and Telemetry
Description
The Multi-Service Data Link (MSDL) transponder is a command receiver, digital command
decoder, digital telemetry encoder, telemetry transmitter, and target interface enclosed in a single
lightweight package. The transponder receives commands transmitted by the ground control station
and interfaces with the vehicle management computer or autopilot.
Uplink UHF command messages from the ground control station are received by the transponder
in the frequency band of 359.5 MHz to 375 MHz. The RF data is converted to a serial data stream
that is digitally transmitted to the vehicle autopilot for processing. The autopilot can then send a
serial data stream back to the transponder where the telemetry downlink is then transmitted down to
the ground control station. The MSDL has three antenna ports to support multiple antenna inputs via
the vehicle RF switch. Multiple antenna inputs can be toggled through for the strongest signal.
MSDL has also been qualified per MIL-STD-461 (EMI), MIL-STD-810 (Environmental), MILHDBK-781 (Reliability) making it one of the most capable devices in the industry.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Characteristics
Frequency:
Channels:
Channel Bandwidth:
Occupied Bandwidth:
Modulation:
Burst Data Rate:
Power Output:
Maximum PRF:
359.5 to 375 MHz
99 (programmable in 25kHz steps)
2.75 MHz
263 kHz
GMSK
230.4 kbps
Up to 35 watts
10 Hz
UHF Receiver
Sensitivity:
Selectivity:
Spurious Rejection:
Greater than 97.5% @ -103 dBm
-60 dBm @ 15.5 MHz
-80 dB
Environmental
Operating: -40 C to +71 C
Random, 20 to 2000 Hz, 11.514 G 48 minutes per orthogonal axis
50,000 ft
Sawtooth, 20 G for 11ms, 18 shocks total
Up to 95% @ 40 C (all boards are conformal coated)
Certified to MIL-STD-461F
Temperature:
Vibration:
Altitude:
Shock:
Humidity:
EMI/RFI:
Power Requirements
DC Power:
Reverse Polarity:
Power Consumption:
22 VDC to 32 VDC (28 VDC Nominal)
Yes
55 Watts maximum (1.8 amps @ 28 VDC)
Physical
Size:
Weight:
Connectors:
Finish:
Installation:
5.00" W x 2.95" T x 6.00" D
6 pounds
Circular, SMA Female
Black Paint
Flange Mount Base Plate
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
© 2010 Micro Systems, Inc
Specifications subject to change without notice
CAP Node
Data Sheet
AS9100C and ISO 9001:2008 Certified
Common Avionics Package (CAP) Node
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Field Proven Hardware
Modular Design
Built-in Autopilot/INS, IMU, GPS and
Datalink processor, and UHF Radio
16 Available Frequency Channels in
the range of 380 MHz to 400 MHz
GMSK Modulation
4 Watt RF Output Power
Includes Analog and Discrete I/O
3 CAN Bus Interface Ports
Meets CDA 101 Specification
Applications
Vehicle Control System
Autopilot
Command and Telemetry
Vehicle Payload Interface
Remote Data Terminal
Description
The Micro Systems Inc. Integrated Avionics Package (IAP) Common Avionics Package (CAP)
Node is a high integration autopilot.
The CAP Node, when used in conjunction with the AFT and Forward (FWD) nodes, supplies the
required signals to enable positive flight control and ancillary systems and payload control of the
MQM-107 Aerial Target Vehicle. It incorporates a UHF datalink, GPS receiver, tactical grade Inertial
Measurement Unit (IMU), and high performance processing electronics in a single high integration
chassis. The CAP Node replaces the functions of the Digital Autopilot (DAP), Vertical Gyro, Yaw
Rate Gyro, Pendulum, and Signal Processor Vehicle Interface (SPVI) as well as the SPVI functions
that process the command and control data link for target control.
The CAP Node Utilizes a Controller Area Network (CAN) Bus for data communications within the
target between multiple components and subsystems. This interface meets the Common Digital
Architecture (CDA) 101 series of specifications.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
21
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Characteristics
Datalink Processor:
Frequency:
Channels:
Channel Bandwidth:
Occupied Bandwidth:
Modulation:
Command Data Format:
Burst Data Rate:
Transmit Power:
Maximum PRF:
UHF Antenna Switch:
CAN Bus:
Receiver Sensitivity:
Receiver Selectivity:
Spurious Rejection:
Interfaces with MSI Upgraded Target Tracking Control System (TTCS/U)
380 MHz to 400 MHz
16
25 kHz
20 kHz
GMSK
RS-232 Asynchronous Serial Data
14.4 kbps
4 Watts
10 Hz
Switching between upper and lower antennas for reliable communications
Adheres to CDA 101 Specifications
-100 dBm @ 1x10-4 BER
-60 dBm @ 12.5 kHz
-70 dB
Input/Output Signals
Analog Inputs:
Analog Outputs:
Discrete Inputs:
Discrete Outputs:
+/- 10 VDC at 12 bit resolution, 4 ports
+/- 10 VDC at 12 bit resolution, drive capacity 10 mA (max), 4 ports
Diode protected, 2 VDC to 35 VDC Active, 0.8 VDC in active, 4 ports
28 VDC/Open output, 2 Amp to resistive load, 0.5 amp to inductive load, 4 ports
Environmental
Temperature:
Cooling:
Vibration:
Altitude:
Shock:
Acceleration:
Humidity:
MTBF:
MTBCF:
Operating: -40 C to +71 C, Non-Operating: -40 C to +85 C
Passive Conductive (no moving parts)
Random, 0.04 G2/Hz 20 – 20,000 Hz, 6 dB/Hz per orthogonal axis
Sea level to 55,000 ft
15 G for 11ms, 18 shocks total
7.5 G constant in any axis
Up to 100% (all boards are conformal coated)
> 1000 Hrs
> 1500 Hrs
Power Requirements
DC Power:
Protection:
Power Consumption:
22 VDC to 32 VDC (28 VDC Nominal)
Surge, Reverse, and Over Voltage protected
100 Watts maximum
Physical
Size:
Weight:
Connectors:
Finish:
Installation:
6.60" W x 5.25" T x 12.31" D
6 pounds
MIL-C38999
Black Paint
Flange Mount Base Plate
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
22
© 2010 Micro Systems, Inc
Specifications subject to change without notice
Forward Node
Data Sheet
AS9100C and ISO 9001:2008 Certified
IAP Forward Node
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Provides +28VDC to main vehicle
power bus
Provides +28VDC and ± 15VDC to
onboard payloads
Multiple CAN bus interface ports
Meets CDA 101 Series Specification
Supports Digital and Analog Payload
Control and Telemetry Interfaces
Interfaces with vehicle Power
Conditioning Unit, Radar Altimeter
and Air Speed Sensor
Applications
Vehicle Control System
Payload Interface
Power Distribution
Description
The Forward (FWD) Node is a general purpose Input/Output (I/O) node for interface and control
of legacy target vehicle positive flight control, ancillary subsystems and payload control of the MQM107E Aerial Target Vehicle.
The FWD Node replaces the functions of the Command Power Distribution Unit and the Payload
Power Distribution Unit. This node provides the power source for the MQM-107E main +28 VDC
target bus. The IAP FWD Node replaces the Signal Processor Vehicle Interface (SPVI) functions
that process commands and telemetry for target control and payload functions located in the forward
section of the target. The FWD Node Utilizes a Controller Area Network (CAN) Bus for data
communications within the target between multiple components and subsystems. This interface
meets the Common Digital Architecture (CDA) 101 series of specifications.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
23
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Electrical
Analog Inputs:
Analog Outputs:
Discrete Inputs:
Discrete Outputs:
CAN Bus:
+/- 10VDC. 0-5VDC at 12 bit resolution
+/- 10VDC, 0-5VDC at 12 bits resolution, maximum drive capacity 10mA
Diode protection, 0.8 VDC inactive, 2 to 35 VDC active
+ 28 VDC/open output, 2 amp to resistive load, 0.5 amp to inductive load
Short circuit protection without damage
Open = >10 Megaohms impedance to ground
Minimum load = 200 mA
Adheres to CDA 101 Specifications
Environmental
Temperature, Operating:
Temperature, Storage:
Random Vibration:
Altitude:
Acceleration:
Shock:
Humidity:
-40°C to +71°C
-40°C to +85°C
Operating, 0.4 G2/Hz 20 Hz - 2000Hz 6 dB/Hz
Sea level to 55,000 feet
7.5G constant in any axis
15G, 11 millisecond duration
100%
Power Requirements
Input Voltage:
Protection:
Power Conditioning Unit (PCU):
Power Consumption:
22 VDC to 32 VDC (+28 VDC nominal)
Reverse Polarity Protected
Rectifies and filters Target Alternator AC, 8 amps maximum total
Distributes +28 VDC to Target Power Bus for Target elements, Aft Node and
CAP node
Provides +/- 15 VDC ( +/- 1%) 400 mA Internal, +/- 100 mA External
Provides + 5 VDC( +/- 1%) 500 mA Internal
25 Watts maximum
Physical
Dimensions:
Weight:
Connectors:
8.4" L x 4.8" W x 4.5" H
Approximately 4 pounds
J1 = MS27468T23B55P
J2 = MS27468T17B35PB
J3 = MS27468T17B35PA
J4, J5, J6 = MS27468T11B5P
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
24
© 2010 Micro Systems, Inc
Specifications subject to change without notice
AFT Node
Data Sheet
AS9100C and ISO 9001:2008 Certified
IAP AFT Node
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Powered by +28VDC Main Target
Power Bus
Provides +28VDC, ± 15VDc, +5VDC
to aft items such as actuators and
parachute deployment equipment
Meets CDA 101 Series Specification
Supports Digital and Analog Payload
Control/Telemetry Interfaces
Interfaces with Electro-Explosives
Device (EED) and Engine Fuel
Control Module
Applications
Vehicle Recovery System
Payload Interface
Engine Control Interface
Description
The AFT Node is a general purpose Input/Output (I/O) node for interface and control of legacy
target vehicle positive flight control, ancillary subsystems and payload control of the MQM-107E
Aerial Target Vehicle.
The AFT Node replaces the functions of the Electro-Explosive Device (EED) Controller and the
Engine Fuel Control Module. This node provides the power source for the MQM-107E main +28
Voltage Direct Current (VDC) target bus. The AFT Node replaces the Signal Processor Vehicle
Interface (SPVI) functions that process commands and telemetry for target control and payload
functions located in the aft section of the target.
The AFT Node Utilizes a Controller Area Network (CAN) Bus for data communications within the
target between multiple components and subsystems. This interface meets the Common Digital
Architecture (CDA) 101 series of specifications.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
25
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Electrical
Analog Inputs:
Analog Outputs:
Discrete Inputs:
Discrete Outputs:
CAN Bus:
+/- 10 VDC. 0 – 10 VDC, 0 – 5 VDC at 12 bit resolution Load Resistance
Conversion 15 ohms to 95 ohms, 12 bits, 10 mA source
+/- 10 VDC, 0 – 5 VDC at 12 bits resolution, maximum drive capacity 10 mA
Diode protection, 0.8 VDC inactive, 2 VDC to 35 VDC active
28 VDC/open output, 2 or 4 amp to resistive load, 0.5 amp to inductive load
Short circuit protection without damage
Open = >10 Megaohms impedance to ground
12 VDC/ground output trigger voltage
12 VDC/open, source 50 mA
DPDT Relay 5 amp, 28 VDC 750 mA Resistive, 200 mA Inductive
Adheres to CDA 101 Specifications
Environmental
Temperature, Operating:
Temperature, Storage:
Random Vibration:
Altitude:
Acceleration:
Shock:
Humidity:
-40°C to +71°C
-40°C to +85°C
Operating, 0.4G2/Hz 20 Hz – 2000 Hz 6 dB/Hz
Sea level to 55,000 feet
7.5 G constant in any axis
15G, 11 millisecond duration
100%
Power Requirements
Input Votage:
Power Conditioning Unit (PCU)
Power Consumption:
22 to 32 VDC, Reverse Polarity Protected, + 12 VDC Recovery Battery
Provides +/- 15 VDC (+/- 1%), + 5 VDC at 12 bit resolution
25 Watts maximum
Physical
Dimensions:
Weight:
5.5" W x 10.8" L x 2.0" H
Approximately 3 pounds
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
26
© 2010 Micro Systems, Inc
Specifications subject to change without notice
Model 290
Data Sheet
AS9100C and ISO 9001:2008 Certified
Model 290 UHF Datalink Transponder
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Field Proven Hardware
Modular Design
16 Available Frequency Channels in
the range of 380 MHz to 450 MHz
GMSK Modulation
Greater than 3W RF Output Power
3 antenna ports
Ruggedized Aluminum Chassis
Applications
Autopilot Interface
Command and Telemetry
Description
The Model 290 UHF datalink transponder is a command receiver, digital command decoder,
digital telemetry encoder, telemetry transmitter, and target interface enclosed in a single lightweight
package. The transponder receives commands transmitted by the ground control station and
interfaces with the vehicle management computer or autopilot.
Uplink UHF command messages from the ground control station are received by the transponder
in the frequency band of 380 MHz to 435 MHz. The RF data is converted to a serial data stream that
is digitally transmitted to the vehicle autopilot for processing. The autopilot can then send a serial
data stream back to the transponder where the telemetry downlink is then transmitted down to the
ground control station. It also has three antenna ports to support multiple antenna inputs via the
vehicle RF switch. Multiple antenna inputs can be toggled through for the strongest signal.
The Model 290 has been qualified per MIL-STD-461 (EMI), MIL-STD-810 (Environmental), MILHDBK-781 (Reliability) making it one of the most capable devices in the industry.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Characteristics
Frequency:
Channels:
Channel Bandwidth:
Occupied Bandwidth:
Modulation:
Burst Data Rate:
Power Output:
Maximum PRF:
Model 290-1: 435 MHz to 450 MHz | Model 290-2: 380 MHz to 400 MHz
16
25 kHz
20 kHz
GMSK
14.4 kbps
Greater than 3 Watts
10 Hz
UHF Receiver
Sensitivity:
Selectivity:
Spurious Rejection:
-100 dBm @ 1x10-4 BER
-60 dBm @ 12.5 kHz
-70 dB
Environmental (MIL-STD-810) / EMI (MIL-STD-461D)
Operating: -40 C to +71 C
Random, 15 to 2000 Hz, 9.3 G 30 minutes per orthogonal axis
50,000 ft
Sawtooth, 20 G for 11ms, 18 shocks total
Up to 95% @ 40 C (all boards are conformal coated)
Certified to MIL-STD-461D, Class A1
Temperature:
Vibration:
Altitude:
Shock:
Humidity:
EMI/RFI:
Power Requirements
DC Power:
Reverse Polarity:
Power Consumption:
22 VDC to 32 VDC (28 VDC Nominal)
Yes
55 Watts maximum (1.8 amps @ 28 VDC)
Physical
Size:
Weight:
Connectors:
Finish:
Installation:
5.00" W x 2.95" T x 6.00" D
6 pounds
Circular, SMA Female
Black Paint
Flange Mount Base Plate
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
© 2010 Micro Systems, Inc
Specifications subject to change without notice
Model 280-1
Data Sheet
AS9100C and ISO 9001:2008 Certified
MONTAGE Transponder – Model 280-1
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Field Proven Hardware
Modular Design
16 Available Frequency Channels in
the range of 435 MHz to 450 MHz
GPS Receiver
GMSK Modulation
4 Watt RF Output Power
Ruggedized Aluminum Chassis
Qualified to MIL-STD-461D (EMI),
MIL-STD-810 (Env)
Applications
Autopilot Interface
Command and Telemetry
Vehicle Payload Interface
Description
The Model 280-1 MONTAGE Transponder is a command receiver, digital command decoder,
digital telemetry encoder, telemetry transmitter, and target interface enclosed in a single lightweight
package.
The transponder receives commands transmitted by the controlling station or the target drone
set. Implementation of commands occurs only after verification of the address, parity, and message
integrity checks. After verifying the address in the command uplink message, the transponder
initiates the transmission of a telemetry reply. The self contained GPS receiver provides excellent
position accuracy during all vehicle maneuvers.
The Model 280-1 allows multiple targets to be flown on the same frequency and can be used as a
target relay. This transponder is currently used on the U.S. Navy’s family of target vehicles including
the BQM-34 and BQM-74 aerial targets, MST-35 and HSMST sea surface targets, and international
vehicles like the Chukar III.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
29
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Characteristics
Frequency:
Channels:
Channel Bandwidth:
Occupied Bandwidth:
Modulation:
Burst Data Rate:
Power Output:
Maximum PRF:
435 MHz to 450 MHz
16
25 kHz
20 kHz
GMSK
14.4 kbps
4 Watts
10 Hz
UHF Receiver
Sensitivity:
Selectivity:
Spurious Rejection:
-100 dBm @ 1x10-4 BER
-60 dBm @ 12.5 kHz
-70 dB
GPS Receiver
Position Update Rate:
Accuracy:
Differential Corrections:
Time to First Fix:
Tracking:
10 Hz
5m CEP
RTCM V2.3
90 seconds
Up to 20 G
Environmental (MIL-STD-810) / EMI (MIL-STD-461D)
Operating: -40 C to +71 C
Passive Conductive (no moving parts)
Random, 15 to 2000 Hz, 9.3 G 30 minutes per orthogonal axis
50,000 ft
Sawtooth, 20 G for 11ms, 18 shocks total
Up to 95% @ 40 C (all boards are conformal coated)
Certified to MIL-STD-461D, Class A1
Temperature:
Cooling:
Vibration:
Altitude:
Shock:
Humidity:
EMI/RFI:
Power Requirements
DC Power:
Reverse Polarity:
Power Consumption:
22 VDC to 32 VDC (28 VDC Nominal)
Series diode protection
55 Watts maximum (1.8 amps @ 28 VDC)
Physical
Size:
Weight:
Connectors:
Finish:
Installation:
10.0" W x 4.25" T x 8.50" D
7.8 pounds
MIL-C38999
Black Paint
Flange Mount Base Plate
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
30
© 2010 Micro Systems, Inc
Specifications subject to change without notice
TCT
Data Sheet
AS9100C and ISO 9001:2008 Certified
Target Control Transponder (TCT)
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Dual mode (command and track)
2 proportional and 24 discrete uplink
commands
12 proportional and 12 discrete
downlink telemetry
Command error probability less than
0.82 x 10-8
Failure alarm circuitry
Automatic antenna selector switch
for two-antenna operation
100 dB receiver dynamic range
Automatic gain control
Pulse width discrimination
Pulse amplitude discrimination
Applications
Command and Control
Command and Telemetry
Description
The Target Control Transponder provides command and control capability, position data and
telemetry data for Unmanned Aerial Vehicles (UAV’s) and Targets when used with the HVS Model
6157-1 Portable Radar Tracking and Control System (PRTCS) or 6104 Transportable Tracking and
Control System (TTCS).
Two modes of operation (Command and Track) are available. In the Command mode, PulsePosition-Code (PPC) interrogations are transmitted by the Ground System. This 5-pulse group is
received and decoded by the transponder set and commands are output to the vehicle. The
transponder set can simultaneously respond to command mode and track mode interrogations and
output both 4-pulse and 2-pulse coded PPC.
The design employs the latest in devices, circuitry, and modern production processes to provide
a reliable product with high quality consistency. This unit is intended for programs and applications
with stringent environmental, EMI, and reliability requirements.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
31
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Electrical
Receiver
Primary Power: 22 to 29 Volts DC
Power Consumption: 4.0 amp, maximum @ 28 Volts DC
Reference Voltage: 5.0 +0.03 VDC at 50 ma
Frequency Separation (Receiver/Transmitter): 50 MHz, minimum
Transponder Delay: 4.0 +0.1 microsecond
Command Functions: 2 Proportional, 8-bit, standard TTL output drive;
24 Discrete, active-on, standard TTL output drive
Telemetry Functions: 12 Proportional, 0 to +5 Vdc input with 10-bit
resolution, 500 K input impedance; 2 Discrete, TTL-compatible inputs
with ON/OFF resolution, 20 K input impedance
Pulse Repetition Rate: 1280 pps minimum, 4160 pps maximum
VSWR of Load: Operate into VSWR of 1.5:1 at all phase angles
Type: Solid State Superheterodyne
Sensitivity (99% Reply): -80 dBm minimum
Frequency Range: 5.4 to 5.9 GHz (tunable)
Frequency Stability: +5 MHz
Dynamic Range: +20 to -80 dBm
Bandwidth: 13 +5 MHz
Interrogation Code: Command, 5-pulse (PPC); Track, 2-pulse
AGC Dynamic Range: 40 dB, minimum
Pulse Width Discriminator: 0.20 to 0.60 +0.05 microsecond for
signal levels 0 to -67 +3 dBm
Pulse Amplitude Discriminator: Varies inversely with AGC level
Transmitter
Physical
Type: Pulsed Magnetron
Frequency Range: 5.4 to 5.9 GHz (tunable)
Frequency Stability +6 MHz
Peak Power Output: 600 Watts, minimum
Pulse Width: 0.3 +0.1 microsecond
Pulse Rise Time: 0.1 microsecond, maximum, (10 to 90%)
Pulse Fall Time: 0.2 microsecond, maximum, (90 to 10%)
Leading Edge Jitter: +0.1 microsecond pulse-to-pulse
Reply Code: Telemetry 4-pulse (PPC); Track, 2-pulse
Size: 4.06 x 10.65 x 8.69 inches, with protrusions
Weight: 13 pounds, maximum
Antenna Connector: N female (MIL-C-39012)
Antenna Switch: Automatic selection of antenna by TCT
Power Connector: Mates with MS3116F12-10S
Telemetry Connector: Mates with MS3116F18-32S
Command Connector: Mates with MS3116F22-55S
Environmental
Options
Vibration: IAW MIL-STD-810C, Method 514.2, Category (e),
Procedure V as follows: Part 1: Sinusoidal-Curve P (5.0g maximum);
Part 2: Random-Curve AF (7.6g)
Temperature, Operating: -40 C to +55 C (+71 C intermittent)
Temperature, Non-Operating: -57 C to +85 C
Shock: 15g for 11 millisecond, IAW MIL-STD-810C, Method 516.2,
Figure 516.2-2, Procedure I
Altitude: 50,000 feet and continuous sea-level operation over -40 C
to +55 C
Humidity: 95 +5, -3% at 65 C, IAW MIL-STD-810C, Method 507.1,
Procedure I, Non-Operating
Immersion: Will withstand immersion in water at a 36-inch depth
IAW MIL-STD-810C, Method 512.1, Procedure I
Salt Atmosphere: Will withstand exposure to salt fog
IAW MIL-STD-810C, Method 509.1, Procedure I
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
32
© 2010 Micro Systems, Inc
Specifications subject to change without notice
Model 99-2
Data Sheet
AS9100C and ISO 9001:2008 Certified
Universal Signal Processor - Vehicle Interface (USPVI)
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Field Proven Hardware
Modular Design
16 Available Frequency Channels in
the range of 380 MHz to 400 MHz
GPS Receiver
GMSK Modulation
4 Watt RF Output Power
Ruggedized Aluminum Chassis
Qualified to MIL-STD-461D (EMI),
MIL-STD-810 (Env)
Applications
Autopilot Interface
Command and Telemetry
Vehicle Payload Interface
Description
The Model 99-2 Universal Signal Processor - Vehicle Interface (USPVI) provides the interface
between a UHF Target Tracking Control Station and an on-board vehicle autopilot.
The USPVI receives a command message from a ground control station, evaluates the message
for proper addressing and error detection, then passes the validated commands to the vehicle
autopilot. The USPVI also responds to the ground control station with vehicle performance telemetry.
The USPVI is fully self contained including RF transceiver, high performance GPS receiver, and
processing electronics.
The USPVI is currently used on the MQM-107 D/E sub scale aerial target, BQM-34 sub scale
aerial target, and the QUH-1 full scale rotary wing target. It can be adapted to other vehicles.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
33
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Characteristics
Frequency:
Channels:
Channel Bandwidth:
Occupied Bandwidth:
Modulation:
Burst Data Rate:
Power Output:
Maximum PRF:
380 MHz to 400 MHz
16
25 kHz
20 kHz
GMSK
14.4 kbps
4 Watts
10 Hz
UHF Receiver
Sensitivity:
Selectivity:
Spurious Rejection:
-100 dBm @ 1x10-4 BER
-60 dBm @ 12.5 kHz
-70 dB
GPS Receiver
Position Update Rate:
Accuracy:
Differential Corrections:
Time to First Fix:
Tracking:
10 Hz
5m CEP
RTCM V2.3
90 seconds
Up to 20 G
Environmental (MIL-STD-810) / EMI (MIL-STD-461D)
Operating: -40 C to +71 C
Passive Conductive (no moving parts)
Random, 15 to 2000 Hz, 9.3 G 30 minutes per orthogonal axis
50,000 ft
Sawtooth, 20 G for 11ms, 18 shocks total
Up to 95% @ 40 C (all boards are conformal coated)
Certified to MIL-STD-461D, Class A1
Temperature:
Cooling:
Vibration:
Altitude:
Shock:
Humidity:
EMI/RFI:
Power Requirements
DC Power:
Reverse Polarity:
Power Consumption:
22 VDC to 32 VDC (28 VDC Nominal)
Series diode protection
55 Watts maximum (1.8 amps @ 28 VDC)
Physical
Size:
Weight:
Connectors:
Finish:
Installation:
6.50" W x 4.25" T x 11.5" D
8 pounds
D-Subminiture
Black Paint
Flange Mount Base Plate
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
34
© 2010 Micro Systems, Inc
Specifications subject to change without notice
Model 99-8
Data Sheet
AS9100 Rev. C and ISO 9001-2008 Certified
Model 99-8 USPVI
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Field Proven Hardware
Modular Design
16 Available Frequency Channels in
the range of 380 MHz to 400 MHz
GPS Receiver
GMSK Modulation
4 Watt RF Output Power
Ruggedized Aluminum Chassis
Qualified to MIL-STD-461D (EMI),
MIL-STD-810 (Env)
Applications
Autopilot Interface
Command and Telemetry
Vehicle Payload Interface
Description
The Model 99-8 Universal Signal Processor - Vehicle Interface (USPVI) provides the interface
between a UHF Target Tracking Control Station and an on-board vehicle autopilot.
The Model 99-8 receives a command message from a ground control station, evaluates the
message for proper addressing and error detection, then passes the validated commands to the
vehicle autopilot. The Model 99-8 also responds to the ground control station with vehicle
performance telemetry. The Model 99-8 is fully self contained including RF transceiver, high
performance GPS receiver, and processing electronics.
The Model 99-8 is currently used on the MQM-107 D/E sub and BQM-34 sub scale aerial targets.
It can be adapted to other vehicles with customer provided interface definitions.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
35
Technical Specifications
AS9100 Rev. C and ISO 9001-2008 Certified
Characteristics
Frequency:
Channels:
Channel Bandwidth:
Occupied Bandwidth:
Modulation:
Burst Data Rate:
Power Output:
Maximum PRF:
380 MHz to 400 MHz
16
25 kHz
20 kHz
GMSK
14.4 kbps
4 Watts
10 Hz
UHF Receiver
Sensitivity:
Selectivity:
Spurious Rejection:
-103 dBm @ 1x10-4 BER
-60 dBm @ 12.5 kHz
-70 dB
GPS Receiver
Position Update Rate:
Accuracy:
Differential Corrections:
Time to First Fix:
10 Hz
Less than 50cm typical horizontal RMS
RTCM V2.3
45 seconds
Environmental (MIL-STD-810) / EMI (MIL-STD-461D)
Operating: -40 C to +71 C
Passive Conductive (no moving parts)
Random, 15 to 2000 Hz, 9.3 G 30 minutes per orthogonal axis
50,000 ft
Sawtooth, 20 G for 11ms, 18 shocks total
Up to 95% @ 40 C (all boards are conformal coated)
Certified to MIL-STD-461D, Class A1
Temperature:
Cooling:
Vibration:
Altitude:
Shock:
Humidity:
EMI/RFI:
Power Requirements
DC Power:
Reverse Polarity:
Power Consumption:
22 VDC to 32 VDC (28 VDC Nominal)
Series diode protection
55 Watts maximum (1.8 amps @ 28 VDC)
Physical
Size:
Weight:
Connectors:
Finish:
Installation:
6.50" W x 4.25" T x 11.5" D
8 pounds
D-Subminiture
Black Paint
Flange Mount Base Plate
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
36
© 2010 Micro Systems, Inc
Specifications subject to change without notice
IFC
Data Sheet
AS9100C and ISO 9001:2008 Certified
Integrated Flight Controller (IFC)
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Field Proven Hardware
High performance PowerPC based
single processor design
Capable of processing up to 64
uplink discrete and 20 proportional
commands
Capable of providing up to 32
discrete & 32 proportional telemetry
channels
Communication with Control
Datalink Transponder via RS-485
RS-422 interface to APS, Umbilical,
ECU, IFF, & ALE 47 Sequencers
Applications
Vehicle Control System
Autopilot
Command and Telemetry
Vehicle Payload Interface
Description
The Integrated Flight Controller (IFC)/Message Processor contains the datalink encode/decode
and autopilot functions. These two functions are performed by a single high performance PowerPC
processor. The IFC provides autonomous control functions to assure safe operation of the aircraft in
the event of command datalink loss. This includes recovery to stable flight conditions while
performing commanded maneuvers and control for escape maneuvers of individual drones under all
flight conditions.
The IFC communicates with the Control Datalink Transponder via EIA RS-485 serial interfaces.
The IFC receives uplink commands from the ground control station and outputs control signals the
UAV . The IFC transmits downlink telemetry information (UAV performance information) to the
ground control station.
The IFC/Message Processor communicates with the attitude sensor package (ASP) via EIA RS485 at a 100 Hz rate. The IFC gathers Heading, Pitch Angle, Roll Angle, Pitch rate, Roll rate, and
Yaw rate from the ASP. The IFC/Message Processor communicates to Ground Support Equipment
(GSE) via an EIA RS-422 serial umbilical interface. This interface is used to load initialization
parameters and flight information in to the IFC. This interface is also used to connect to the Target
Test Set.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
37
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Characteristics
IFC Address:
Interrogation Rate:
Discrete Commands:
Proportional Commands:
Discrete Telemetry:
Proportional Telemetry:
Command Interface:
APS Interface:
GSE Interface:
Spare:
Front panel programmable
100 milliseconds (10 command/telemetry messages per second)
64, GND closure of up to 20, 12 bit channels
Capability of up to 20, 12 bit channels
32, Open/GND/5 VDC
Capability of up to 6 channels 16 bit and 16 channels 10 bit inputs
EIA RS-485
EIA RS-485 @ 100 Hz
EIA RS-422
Discrete, Proportional, CANbus and serial interfaces for future expansion
Environmental
Temperature:
Cooling:
Vibration:
Altitude:
Shock:
Humidity:
Acceleration:
Operating: -40 C to +71 C Storage: -54 C to +125 C
Passive Conductive (no moving parts)
Operating, Random, 0.15g2/Hz, 20Hz to 100Hz
Operating, Random, 0.04g2/Hz 100Hz to 2000 Hz for 5 minutes per orthogonal axis (8.8 Grms)
Sea Level to 50,000 ft
Half Sine, 20 G’s peak, 11 ms, 3 axes
Up to 95% @ 40 C (all boards are conformal coated)
10 G’s, 3 axes, tested at drone level
Power Requirements
DC Power:
Input Current:
Protection:
22 to 32VDC (28VDC Nominal)
0.5 Amps maximum
Reverse polarity protected
Physical
Size:
Weight:
Installation:
9.30" W x 4.25" T x 2.51" D
4 pounds
Flange Mount Base Plate
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
38
© 2010 Micro Systems, Inc
Specifications subject to change without notice
PMU
Data Sheet
AS9100C and ISO 9001:2008 Certified
Power Management Unit (PMU)
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Field Proven Hardware
Operates with 28 VDC input from
Power Conditioning Unit, Umbilical,
& Battery
Provides 28 VDC battery backed
power to the avionic components
Provides switched power to servos,
fuel system, & payloads
Applications
Vehicle Power Management System
Description
The Power Management Unit (PMU) is suitable for use on Aerial Targets and UAVs to distribute
switched and un-switched power (+28 VDC & Ground) to the various avionic and payload
components. The PMU utilizes the latest in modem devices and circuitry to provide a reliable product
with an extremely long operating life.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
39
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Characteristics
Power Consumption:
Temperature:
Cooling:
Vibration:
Shock:
Altitude:
<1.5 amps @ 28 VDC
Operating: -40 C to +71 C Storage: -54 C to +125 C
Passive Conductive (no moving parts)
Operating, Random, 10 GRMS
Half Sine, 20 G’s peak, 11 ms, 3 axes
Up to 50,000 feet
Capabilities
Operates with 28 VDC input from:
- Power Conditioning Unit
- Umbilical
- Battery
Provides 28 VDC battery backed power to the avionic components of the air vehicle including but not limited to:
- Fuel control system including Main Flow Meter and Linearizer
- Transfer Flow Meter and Linearizer
- Fuel Quality Sensor
- Fuel Boost Pump
- APS, Radar Altimeter, Command & Control Transponder, Engine Control Unit, Antenna Switch, EED, GPS
antenna, IFC, Pitot Heaters and IFF Transponder
Provides switched power to:
- Servo actuators including Rudder, Stabilator, Aileron, & Speed Brakes
- Fuel Pumps, Air Data Module, Strobe Light, Engine Igniter, & Scoring
- Payload components including APC-4 (up to 10 amps @ 28 VDC) for future payload use
- PMU provides spare switched power (5 amp, 12 amp, & 25 amp) for future payload use
- Accepts Discrete commands from the Integrated Flight Controller (IFC) to provide switched power to the
onboard components
Physical
Size:
Weight:
Installation:
9.75" W x 4.82" T x 6.00" D
11 pounds
Flange Mount Base Plate
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
40
© 2010 Micro Systems, Inc
Specifications subject to change without notice
EED
Data Sheet
AS9100C and ISO 9001:2008 Certified
Electro-Explosive Device (EED) Controller
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Field Proven Hardware
Operates with 28 VDC input and 12
VDC input from Power Management
Unit (PMU)
Receives Drogue Deploy from PMU
Receives Loss of Command
Present signal from Integrated Flight
Controller (IFC)
Receives Emergency Parachute
Activation from IFC
Applications
Vehicle Recovery System
Description
The Electro-Explosive Device (EED) Controller is suitable for use on Aerial Targets and UAV’s to
enable the orderly deployment of the parachutes in order to safely recover the vehicle. The unit
provides timing circuits for recovery system arming, the main parachute deployment delay, and
automatic and commanded recovery sequences. It controls power to the explosive cartridges used
to deploy and release the parachute and tow target systems and deactivation of power to the
avionics suite. The EED utilizes the latest modem devices and circuitry to provide reliable a product
with an extremely long operating life.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
41
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Characteristics
Input Voltage Range:
Power Consumption:
Temperature:
Cooling:
Vibration:
Shock:
Altitude:
24 VDC to 32 VDC (28 VDC Nominal) and 12 VDC +/- 1 VDC
<1 amp @ 28 VDC
Operating: -40 C to +71 C Storage: -54 C to +125 C
Passive Conductive (no moving parts)
Operating, Random, 10 GRMS
Half Sine, 20 G’s peak, 11 ms, 3 axes
Up to 50,000 feet
Capabilities
Recovery Initiation:
- Emergency Parachute Release: Manual activation fo the recovery and tail cone release sequence
- Command Signal Loss: Automatic recovery sequence initiation upon Loss of Command (IFC OK)
- Low Voltage: Automatic recovery sequence initiation upon detection of a low voltage of 22 +/- 1 VDC
- Drogue Deploy: Automatic recovery sequence initiation upon Loss of regulated 15 VDC power or 28 VDC
Drogue Deploy
Recovery Arm (Telemetry)
- The downlink telemetry data for the recovery arm: 3.5 +/- VDC
Provides switched power to:
- Orderly activation of the Squibs, Bag Line Cutters, and Chute Release Circuit armaments
- Organized chute release switch activation, chute release Squib firing, and final deactivation of the power to
the avionics components of the vehicle
Physical
Size:
Weight:
Installation:
9.30" W x 4.125" T x 2.51" D
3.5 pounds
Flange Mount Base Plate
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
42
© 2010 Micro Systems, Inc
Specifications subject to change without notice
GRDCS
Data Sheet
AS9100C and ISO 9001:2008 Certified
GRDCS/DFCS RF Transponder
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Operates with single power supply
Designed for extended temperature
range
Power consumption > 70 Watts
Bi-phase modulated 915 MHz
Transmit/Receive
Direct Sequence Spread Spectrum
(DSSS)
Peak output power of 200 Watts
Communication to IFC via RS-485
Channel
Applications
Vehicle Tracking
Distance Measurement Equipment
Description
The Gulf Range Drone Control System (GRDCS) / Drone Formation Control System (DFCS) RF
Transponder is an L-Band transmitter/receiver designed to function as a Distance Measuring
Equipment (DME) to support GRDCS/DFCS navigation requirements.
The use of Time-Of-Arrival (TOA) measurements to compute distances requires the transponder
to reply to uplinked command messages from ground control stations with precisely timed downlink
telemetry messages. The update rate for the datalink messages is nominally 10 messages/second.
The GRDCS/DFCS RF Transponder is capable of interrogation rates form 20 Hz (50 milliseconds) to
2 Hz (500 miliseconds).
The GRDCS/DFCS RF Transponder supports datalink message communication by decoding and
transferring uplink command data to the Integrated Flight Controller (IFC) system, and by encoding
downlink telemetry data representing aircraft flight control mode status and sensor readings from the
IFC. The GRDCS/DFCS RF Transponder communicates with the IFC via EIA RS-485
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
43
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Characteristics
Input Voltage:
Power Consumption:
Data Message Format:
GRDCS Address:
Drone Delay:
Modulation:
Transmit Frequency:
Transmit Frequency Stability:
Duty Cycle:
Receive Center Frequency:
Receive Center Frequency Stability:
Deceive Dynamic Range:
Receive Image Rejection:
RF Input:
IFC Interface:
+24 +/- 0.5 VDC to +32 +/- 0.2 VDC (+28VDC Nominal)
70 Watts maximum
GRDCS message format
9 Bits
(1 to 31) X (0.5 ms)
Bi-phase modulation, Direct Sequence Spread Spectrum (DSSS)
915 MHz (L-Band)
+10 ppm over operating temperature range
2.0 % indefinitely
915 MHz (L-Band)
+10 ppm over operating temperature range
91 dB minimum
60 dB minimum
Maximum +53 dBm at a maximum of 2.0 percent
EIA RS-485
Environmental
Random Vibration:
Temperature:
Cooling:
Shock:
Altitude:
Humidity:
Operating: 0.015g2/Hz 20 to 100 Hz
0.04g2/Hz 100 to 2000 Hz for 5 minutes in each orthogonal direction (8.8 Grms)
Operating: -40 C to +71 C Storage: -54 C to +125 C
Passive Conductive (no moving parts)
Half Sine, 20 G’s peak, 11 ms, 3 axes
Sea level up to 50,000 feet
To 95% at any temperature forming frost or condensation
Physical
Size:
Weight:
Connectors:
9.75" W x 7.42" T x 4.00" D
less than 13 pounds (excluding the mounting brackets)
J1 = TNC; J2 = MS27474Y12B35P
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
44
© 2010 Micro Systems, Inc
Specifications subject to change without notice
MD500L
Data Sheet
AS9100C and ISO 9001:2008 Certified
IFF Transponder Model MD500L
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Operates in 1, 2, 3/A, or C Modes
500 Watt Peak Power Ouput (typ.)
100% Solid State for High Reliability
IFF/TACAN Blanking & Suppression
Interrogation side lobe suppression
for use in busy air corridors
Front panel and remote reply code
selection
Weighs less than 4 pounds
Built-in duplexer for single antenna
operation
Applications
Radar Identification
Vehicle Tracking
Description
The Model MD500L IFF Transponder is an L-Band augmentation device ideally suited for use
in aerial target drones, unmanned vehicles, and cruise missiles as a radar enhancement device to
provide automatic radar identification in response to interrogations from L-Band IFF and Air Traffic
Control (ATC) radars. It also supports Mode C (altitude reporting) operation.
It features a modern compact design with less than 90 cubic inches (1475 cubic centimeters)
volume and weighs 4.25 pounds (1.9 kilograms) which is 35% smaller than previous versions. The
transponder incorporates the latest in solid state electronics design and features a 500 watts nominal
peak power output. It also features IFF/TACAN blanking and suppression, reverse polarity power
lead protection, and has a built in duplexer for single antenna operation. Also, the transponder was
designed with both front panel and remote reply code selection for greater convenience and ease of
use. The L-Band IFF meets the requirements of MIL-STD-810 and is designed to operate over the
temperature range of -54° C to +71°C.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
45
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Electrical
Receiver
Frequency:
1030 / 1090 MHz
Impedance, Input/Output: 50 ohms nominal
Protection:
Built-in series diode
protection against from DC
input power reversal
Input Voltage:
24 to 32 VDC, common GND
Quiescent Current:
0.4 Amp nominal
Input Current:
1.1 Amp typical @ 2500 prf
Input Power:
40 Watts max, all conditions
Suppression Modes:
(1) Decoding suppression during transmission
(2) Interrogation Side Lobe Suppression (ISLS)
(3) Over-interrogation reply limiting
(4) Suppression from an external IFF or TACAN
system
(5) Provides suppression pulse to an IFF or TACAN
system
Direct RF detection & Logarithmic
Amplification
Frequency (3dB): 1027.5 MHz to 1032.5 MHz
(or specify)
Sensitivity:
-69 dBm to -77 dBm, internally
adjustable
Dynamic Range: 50 dB min
Pulse Decoding: Modes externally or remotely
selected
Mode 1 pulse spacing: 3.0 +/- 0.1 secs
Mode 2 pulse spacing: 5.0 +/- 0.2 secs
Mode 3A pulse spacing: 8.0 +/- 0.2 secs
Mode 3C pulse spacing: 21.0 +/- 0.2 secs
Pulse Width (all modes): 0.8 +/- 0.1 secs
Sidelobe Suppression
Pulse:
Positioned 2.0 +/- 0.15 secs
from first pulse. Suppression
occurs when this pulse > in
amplitude to first pulse.
Type:
Environmental
Temp, Operating:
Temp, Storage:
Altitude:
Humidity:
Leakage:
Vibration:
Acceleration:
Shock:
EMI/RFI:
-66 F (-54 C) to 160 F (+71 C)
-80 F (-62 C) to 185 F (+85 C)
Sea Level to 100,000 feet
Any, up to 100% including
condensation due to temperature
change (all boards are conformal
coated)
Water immersion to a depth of 1m for
2 hrs
Random, 9.3 Grms max from 10 to
2000 Hz
20 G in each of 6 direction for 1 min
per axis while operating
20 G (11 ms), 3 shocks each axis
MIL-STD-461, tested per MIL-STD462
Transmitter
Solid-state, silicon bipolar
transistors
Frequency (3dB): 1090 +/- 3 MHz
Power Output:
5 Bit encoded signal between 2
framing pulses spaced 20.3 +/0.1 secs
Pulse Width:
0.45 +/- 0.1 secs
Reply Code
Select:
Front panel switches or remote
Receive to Transmit
Delay:
3.5 secs nominal (jitter 0.1
secs max
Random
Triggering:
5 pulse trains per second max
Type:
Physical
Size:
Weight:
Antenna. Connector:
Pwr/Remote Connector:
IFF/TACAN Connector:
Installation:
5.00" W x 2.52" T x 5.13" D
(12.7 cm x 6.40 cm x 13.03 cm)
4 pounds
TNC Female
MS27474E14B35P
BNC female
Flange Mount Base Plate
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
46
© 2010 Micro Systems, Inc
Specifications subject to change without notice
Model 1000
Data Sheet
AS9100C and ISO 9001:2008 Certified
Model 1000 Radio/Modem
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Frequency: 360 MHz to 380 MHz
800 channels available
20 kHz RF bandwidth
14.4 kbps burst data rate
GMSK modulation
200 NM Line-Of-Sight operation
Operating temperature: -40 C to
71 C
Qualified to MIL-STD-810G (Env)
CANBus, RS232/422/485
Discrete control for antenna
diversity switches
Applications
Military Range Systems
Unmanned Systems
Command and Control
Remote Data Telemetry
Description
The Model 1000 Radio/Modem is a Narrow Band high performance, high reliability datalink
transceiver designed specifically to meet the rigorous demands of Military Range Systems. It
operates in the UHF frequency band of 360 MHz to 380 MHz and supports data rates of up to 14.4
kbps.
The Model 1000 is a cost effective solution that offers performance and versatility in a small form
factor package ideal for OEM applications. It is ideal for the command and control of unmanned
aerial targets, applications for remote data terminal systems, and GPS tracking systems.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
47
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Transmitter
Frequency Range:
Output Power:
Range – Line of Sight:
Modulation:
Occupied Bandwidth:
Channels:
Channel Bandwidth:
Maximum PRF:
360 MHz to 380 MHz
5, 10, and 25 Watt versions available
200 Nautical Miles (NM)
GMSK, 14.4 kbps burst data rate
< 20 kHz
800
25 kHz
10 Hz
Receiver
Sensitivity:
RF Selectivity:
Dynamic Range:
-105 dBm @ 1x10-4 BER
-60 dBm @ 30 kHz
115 dB
Data Transmission
Error Detection:
Error Correction:
Link Throughput:
Data Interface:
Protocol:
Data Connector:
24 or 32 bit CRC
Convolutional Encoding/Viterbi Decoding
14.4 kbps
Serial
RS-232/485/422, CANBus
9 pin D-Subminiature (Female)
Environmental
Temperature:
Cooling:
Vibration:
Altitude:
Shock:
Humidity:
Operating: -40 C to +71 C
Passive Conductive (no moving parts)
Random, 15 to 2000 Hz, 9.3 G 30 minutes per orthogonal axis
50,000 ft
Sawtooth, 20 G for 11ms, 18 shocks total
Up to 95% @ 40 C (all boards are conformal coated)
Power Requirements
DC Power:
Reverse Polarity:
15 VDC Nominal
Series diode protection
Physical
Size – 5 Watt:
Size – 10, 25 Watt:
Weight:
Enclosure:
2.90" W x 3.80" D x 1.43" T
2.90" W x 4.20" D x 1.43" T
0.5 pounds
Optional
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
48
© 2010 Micro Systems, Inc
Specifications subject to change without notice
DLS-r
Data Sheet
AS9100C and ISO 9001:2008 Certified
Data Link System Replacement Transponder
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Operates with single power supply
Designed for extended temperature
range
Applications
GRDCS Transponder
Description
The Data Link Subsystem Replacement (DLS-r) provides the data communications necessary for
remote drone operation in conjunction with the Gulf Range Drone Control System (GRDCS) target
control system.
The DLS-r is used to communicate control commands to a mix of mission participants such as
sub-scale and full-scale drone vehicles, either individually or in a formation. Drone communication
and control is accomplished via uplink/downlink commands sent from the target control system
ground station computer to the DLS-r.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
49
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Characteristics
Input Voltage:
Power Consumption:
Data Message Format:
GRDCS Address:
Drone Delay:
Modulation:
Transmit Frequency:
Transmit Frequency Stability:
Duty Cycle:
Receive Center Frequency:
Receive Center Frequency Stability:
Deceive Dynamic Range:
Receive Image Rejection:
RF Input:
IFC Interface:
+24 +/- 0.5 VDC to +32 +/- 0.2 VDC (+28VDC Nominal)
70 Watts maximum
GRDCS message format
9 Bits
(1 to 31) X (0.5 ms)
Bi-phase modulation, Direct Sequence Spread Spectrum (DSSS)
915 MHz (L-Band)
+10 ppm over operating temperature range
2.0 % indefinitely
915 MHz (L-Band)
+10 ppm over operating temperature range
91 dB minimum
60 dB minimum
Maximum +53 dBm at a maximum of 2.0 percent
EIA RS-485
Environmental
Random Vibration:
Temperature:
Cooling:
Shock:
Altitude:
Humidity:
Operating: 0.015g2/Hz 20 to 100 Hz
0.04g2/Hz 100 to 2000 Hz for 5 minutes in each orthogonal direction (8.8 Grms)
Operating: -40 C to +71 C Storage: -54 C to +125 C
Passive Conductive (no moving parts)
Half Sine, 20 G’s peak, 11 ms, 3 axes
Sea level up to 50,000 feet
To 95% at any temperature forming frost or condensation
Physical
Size:
Weight:
Connectors:
9.75" W x 7.42" T x 4.00" D
less than 13 pounds (excluding the mounting brackets)
J1 = TNC; J2 = MS27474Y12B35P
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
50
© 2010 Micro Systems, Inc
Specifications subject to change without notice
Model 1101
Data Sheet
AS9100C and ISO 9001:2008 Certified
RF Transponder Unit (RTFU)
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Rugged Design
Ground or Airborne
915 MHz
19" Rack Mountable
Applications
GRDCS Ground Station
Airborne Relays
Description
The RFTU is a specialized RF transceiver designed to meet the 915 MHz Gulf Range Drone
Control System (GRDCS) data link requirements of Tyndall Air Force Base (TAFB) and White Sands
Missile Ranges (WSMR). It receives all GRDCS 915MHz transmissions and decodes sync, "A" and
"B" codes within the waveform. It is also transmits a GRDCS message to ground units, airborne
relays and airborne transponders.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
Technical Specifications
AS9100C and ISO 9001:2008 Certified
General
915 MHz + 9.15 kHz
BPSK
TX/RX, 50 ohms type N connector, Maximum VSWR 1.5:1
22-32 VDC (28 VDC Nominal)
< 5 Amps receive only, < 20 Amps transmit (max duty cycle)
Operating Frequency:
Modulation:
Antenna Port:
Operating Voltage:
Operating Current:
Transmitter
915 MHz + 9.15 kHz
-90.0 dBm at volts for temp rng > -40 C to < -20 C
-91.5 dBm w/ obj of -96 dBm, at volts for temp rng > -20 C to < +50 C
-90.0 dBm at volts for temp rng > +50 C to < +71 C
80.0 dBm, span -10dBm to -90 dBm, at volts for temp rng > -40 C to < -20 C
81.5 dBm, span -10dBm to -91.5 dBm, at volts for temp rng > -20 C to < +50 C
80.0 dBm, span -10dBm to -90 dBm, at volts for temp rng > +50 C to < +71 C
60 dB (min)
Operating Frequency:
Receiver Sensitivity:
Receiver Dynamic Range:
Image Rejection:
Receiver
915 MHz + 9.15 kHz
BPSK
> +53 dBm (200W) for temp range > -40 C to < 0 C
> +56 dBm (400W) for temp range > 0 C to < +43 C
> +53 dBm (200W) for temp range > +43 C to < +71 C
20% Maximum
< 1 dB
Operating Frequency:
Modulation:
Transmitter Power:
Duty Cycle:
Power Droop:
Environmental
Temperature:
Vibration:
Operating: -40 C to +71 C Storage: -54 C to +125 C
Random (propeller aircraft)
Physical
Size:
Weight:
16.9" W x 7.0" T x 20.4" D
less than 100 pounds
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
© 2010 Micro Systems, Inc
Specifications subject to change without notice
RADAR TRACKING TRANSPONDERS
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Radar Tracking Transponders (commonly called Tracking Beacons) are extremely small precision
augmentation systems for enhancing the tracking capability of RADAR systems. These transponders
improve the operating distance of a Radar, greatly improves the tracking accuracy, and (when used in
double pulse mode) provide the ability to selectively track a single vehicle out of a group of vehicles.
Micro Systems offers a family of solid state C-Band Radar Tracking Transponders in a variety of output
power levels, package size, and factory or customer programmed.
53
54
Model 25x-x
Data Sheet
AS9100C and ISO 9001:2008 Certified
Programmable C-Band Radar Transponders
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Small footprint ideal for missiles and
smaller unmanned vehicles.
Enhanced Pulse parameter
capabilities
30% smaller than comparable units
Minimum peak power outputs of 20
Watts and 50 Watts
Infinite Shelf Life
Reliable Solid State Transmitter
using the latest GaAs technology
Applications
Vehicle Tracking
Description
The Micro Systems, Inc. families of C-Band Radar Tracking Transponders are compact precision
augmentation systems for enhancing the tracking capability of C-Band Radars. The 50 watt unit is
30% smaller than comparable units. It is particularly suitable for small missiles, targets, and aerial
vehicles where weight and space are of a premium.
These units offer an industry first, offering a reliable solid state transmitter and using the latest in
GaAs technology. The result is low modulation pulse voltages, increased reliability, infinite shelf-life,
and no maintenance requirements. The transmit frequency, receive frequency, and all pulse code
parameters are externally programmable using a standard PC – another industry first. This series of
transponders provides a substantial savings of time and money for testing, systems maintenance,
and operational parameter changes. Minimum peak power outputs of 20, and 50 watts are
available.
Micro Systems, Inc. C-Band Transponders provide enhanced pulse parameter capabilities
incorporating the latest range requirements in an effort to expand the operational capability of
existing C-Band radar systems.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
55
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Transmitter
Frequency:
Minimum Power Output:
Type:
Frequency Stability:
Pulse Width:
PRF:
Reply Delay
5.4 GHz to 5.9 GHz, Externally Programmable at 1 MHz intervals
Model 253-X = 50 Watts; Model 252-X = 20 Watts
Solid State
+/- 3 MHz
250 nsec to 750 nsec ,externally programmable at 50 nsec intervals
Up to 2600 Hz
1 µsec to 9 µsec, externally programmable at 0.5 µsec intervals
Receiver
Frequency:
Sensitivity:
RF Bandwidth:
Pulse Width:
Pulse Decoder:
Pulse Coding:
5.4 GHz to 5.9 GHz, externally programmable at 1 MHz intervals
-65 dBm minimum, ≥99% Reply
11 +/- 3 MHz
0.25 µsec to 5.0 µsec Single pulse, 0.25 µsec to 1.0 µsec Double pulse
Single or Double, externally programmable
2 µsec to 16 µsec externally programmable at 0.5 µsec intervals
Environmental
Temperature, Operating:
Temperature, Storage:
Vibration:
Altitude:
Acceleration:
Shock:
Humidity:
EMI/RFI:
-40°C to +71°C; -54°C to +85°C Available
-62°C to +95°C
MIL-STD-810C
85,000 feet
50 G’s all axis 1 minute
100 G’s all axis 6 msec, 120 G’s all axis 4 msec
100%
MIL-STD-461C, Class A1 equipment, IAW MIL-STD-462
Power Requirements
DC Power:
Reverse Polarity:
Impedance:
Power Consumption:
22 to 34 VDC (28 VDC nominal)
Series diode protection
50 ohms
9 Watts maximum (320 mA @ 28 VDC)
Physical
Size:
Weight:
Volume:
Power Connector:
3.50" W x 1.40" T x 3.95" D (8.9 x 3.6 x 10 centimeters)
18 ounces (510 grams)
18 cubic inches (295 cubic cm)
MS2746Y08D35P
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
56
© 2010 Micro Systems, Inc
Specifications subject to change without notice
Programming Set
Data Sheet
AS9100C and ISO 9001:2008 Certified
C-Band Transponder Programming Set
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
USB Computer Interface
Windows XP and later operating
system compatibility
Program the following parameters in
MSI C-Band Products:
- Transmit Frequency
- Receive Frequency
- Reply Delay
- Pulse Code Type
- Pulse Spacing
- Pulse Width
Applications
MSI C-Band Transponder/Beacon
Programming
Mini-Tester Programming
Description
The Micro Systems, Inc. C-Band Transponder Programming Set provides the user with the
capability to field program the operational parameters of our Models 252 and 253 C-Band Radar
Tracking Transponders. When connected to a user supplied laptop computer, and a compatible
transponder, the programmer enables the user to set the following operational parameters:
Transmit Frequency
Receive Frequency
Reply Delay
Pulse Coding Type (Single or Double Pulse)
Pulse Spacing
Pulse Width
The programming set also enables field programming of the transmit frequency of our Models 382, 38-4, and 38-5 Mini-Testers. Includes software, USB Interface Cable, Programming Cable, and
AC Power Adapter.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
57
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Characteristics
PC Interface:
Compatible with:
Operating System:
USB
Transponders: Model 251-2, 252-2, 252-3, 253-3 | Test Sets: Model 38-2, 38-4, 38-5
Windows XP and later
Environmental
Temperature, Operating: 0°C to +40°C
Temperature, Storage:
-25°C to +65°C
Power Requirements
DC Power:
Reverse Polarity:
Power Consumption:
22 to 34 VDC
Series diode protection
10 Watts maximum
Physical
Size:
Weight:
5" W x 1.5" T x 2.0" D
less than 18 ounces (510 grams)
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
58
© 2010 Micro Systems, Inc
Specifications subject to change without notice
SCORING SYSTEMS
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Micro Systems offers complete scalar (miss distance) air-to-air or sea surface-to-air non-cooperative
scoring systems. No modification is required to the missile. We offer complete, turn-key solutions
including the scoring sensor (air or sea surface vehicle), scoring ground stations, and test sets. The
miss distance sensor (AN/DSQ-50A) is a high performance pulsed Doppler system installed in the
vehicle and detects when a missile passes within the sensor range. The sensor information is then
transmitted to the ground station. The ground station recieves the information and quickly calculates the
miss distance. This calculation can be performed automatically or in operator-assisted mode. The
scoring ground station can also be interfaced to our MONTAGE Command and Control System to
provide automatic, low cost, telemetry receiver antenna tracking.
59
60
AN/DSQ-50A
Data Sheet
AS9100C and ISO 9001:2008 Certified
AN/DSQ-50A Miss Distance Scoring Sensor
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
0 to 75 feet scoring range
1 foot scoring accuracy
Multiple target application
Environmentally qualified to MILSTD-810
EMI qualified to MIL-STD-461
Sea Skimming or High Altitude
Applications
Vehicle Miss Distance Scoring
Description
The Micro Systems Inc. AN/DSQ-50A Miss Distance Sensor is the airborne element of the AN/
USQ-104 RF Scalar Scoring System. Tracking data from the AN/DSQ-50A is transferred in real time
to the Scoring Ground Control System, where it is captured and processed to produce scores for the
user.
The AN/DSQ-50A was designed for the installation in to all US Navy targets to acquire scoring
information on passing projectiles and missiles. This unit is ideally suited for installation in to
subscale targets where available space and weight are a concern. It is a non-cooperative, scalar
miss-distance indicator (MDI) system capable of providing near real-time, accurate miss-distance,
time, and closing velocity data for high altitude and low altitude intercept scenarios.
The AN/DSQ-50A operates against high performance missiles as well as ballistic projectiles as
small as 76 mm. It has the capability to operate in live-fire training mission environments containing
up to six target vehicles, with each vehicle equipped with a MDI system. Each MDI operates without
concern of interference from other MDIs. It consists of two functional elements; and MDI radar
sensor to acquire the scoring information and a telemetry transmitter downlink to send the scoring
information to a ground set.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
61
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Characteristics
Type:
Scoring:
Scoring Rate:
Scoring Range:
Closing Velocity:
Accuracy Miss Distance:
Accuracy Velocity:
RF, Non-cooperative, Scalar
Missiles and Projectiles (76 mm and larger)
90 projectiles per minute
0 to 75 feet (0 to 22.86 meters)
200 to 8,000 ft/sec (60.96 to 2438.4 m/sec)
1.0 ft (rms) for 0 to 75 ft scoring range (0.31 ft)
25 ft/sec (7.62 m/sec or 1% (rms)
Electrical
Radar Transmitter
Frequency:
Power (peak pulse):
Pulse Width:
PRF:
Telemetry
Format:
Bit Rate:
Bandwidth:
Frequency (tunable):
Power:
Number of Targets:
2433.077 – 2433.913 MHz (6 channels)
20 Watts maximum at antenna
220 ns nominal
1 MHz nominal
NRZL
700 kb/s
1 MHz
1435.5 – 1535.5 MHz (L-Band) and 2200.5 – 2289.5 MHz (S-Band)
2 Watts minimum
6 simultaneous max with 200 feet minimum separation
Power Requirements
DC Power:
Consumption:
Protection:
22 to 32 VDC (28 VDC Nominal)
65 Watts max
Reverse polarity protected
Environmental / EMI
Temperature:
Cooling:
Vibration:
Temp/Humidity/Alt:
Shock:
Salt Fog:
Acoustical Noise:
Reliability:
Operating: -40 F to +159 F (-40 C to +71 C)
Non-Operating: -65 F to +203 F (-54 C to +95 C)
Passive Conductive (no moving parts)
MIL-STD-810E, Method 514.4, Equipment Category 5 Procedure I
MIL-STD-180E, Method 520.1, Procedure III
MIL-STD-810E, Method 516.4, Procedure I
MIL-STD-180E, Method 509.3, Procedure I
MIL-STD-180E, Method 515.4, Procedure II
500 hours Mean Time Between Failure (MTBF)
Physical
Size:
Weight:
Installation:
9.06" L x 6.33" W x 3.00" H (23.01 cm x 16.08 cm x 7.62 cm)
9 pounds
Flange Mount Base Plate
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
62
© 2010 Micro Systems, Inc
Specifications subject to change without notice
Scoring System
Data Sheet
AS9100C and ISO 9001:2008 Certified
Turn-Key Scoring System
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Compatible with DSQ-50A scoring
sensor.
Miss Distance results in 5 minutes or
less.
Portable system easily installs at
command center or in any vehicle,
vessel, or aircraft.
Easy to use Graphical User Interface
(GUI)
Rugged Transit Case
Applications
Scoring Ground System
Gunnery Training
Weapon Assessment
Scoring Sensor
DSQ-50
Description
The Micro Systems, Inc has developed an easy-to-use Miss Distance Scoring System that provides high
accuracy scoring with minimal training requirements. The system is a rugged complete scoring solution that is
field proven and ideal for gunnery training and weapons assessment for surface and dynamic airborne targets.
It is a highly portable system that can be easily set up and ready to support mission operations in less than 5
minutes.
Micro Systems offers a complete turn-key scoring system that includes the miss distance scoring ground
system and DSQ-50 scoring sensor. The scoring sensor transmits a Doppler radar signal and then detects the
radar reflection from a projectile as it passes by. The radar reflection data is then telemetered in real-time to
the miss distance ground system which allows the scoring system operator to analyze the data and determine
the miss distance score within seconds. This is a scalar system which enables the operator to determine how
close the projectile actually came to the target.
The Micro Systems scoring system is a necessity for advanced training and weapon assessment. Scoring
data is obtained by the system in seconds which provides for extremely efficient training and evaluation
missions. As a training tool users will get immediate feedback of their firing performance as well as objective
measurement weapon system operator skills. For weapon assessment the system can be used for high
resolution measurement of weapon accuracy allowing for firing adjustments to be made on the spot with little
to no delay.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
63
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Scoring System Data
Time to Display Score:
Range:
Accuracy:
Projectile Passage Range:
Rate:
Minimum Projectile Size:
Closing Velocity:
Time of Miss Distance:
Operator Displays:
Data Storage:
Within 5 minutes of each scoring event
Line Of Sight (LOS) system to 5mi (8km) – dependent on altitude, obstacles, etc.
+/- 1 ft RMS (.30m)
0 to 75 ft (0 to 23 m)
Up to 90 projectiles per minute
From 50 Caliber and up (12.7mm and up)
60 m/s (135 mph) to 2500 m/s (5600 mph)
+/- 0.5 msec
Miss Distance, Time of Miss Distance, Plot of Closing Velocity vs. Time
All raw telemetry data and calculated parameters are stored fro each scoring event
Telemetry Frequency Range:
Telemetry Sensitivity:
Telemetry Demodulation:
1429 MHz to 1545 MHz (L-Band) or 2185 MHz to 2485 MHz (S-Band)
-85 dBm
PCM NRZ-L, Up to 7 Mbps
Temperature:
Input Voltage:
Power:
Dimensions:
Operating: +5 deg C to +40 deg C
115 VAC, Single Phase
200 Watts
19" x 7" x 24.5"
Scoring Sensor – DSQ-50A
Type:
RF, Scalar
Number of Targets:
6 simultaneous max with 200ft minimum separation
Temperature:
Operating: -40 C to +71 C
Input Power:
22 to 32 VDC (28 VDC Nominal) – 65 Watts (max) – Reverse polarity protected
Qualified per MIL-STD-810E:
Vibration, Shock, Temperature, Humidity, Altitude, Salt Fog, and Acoustical Noise
Reliability:
500hrs MTBF
Size:
9.1" x 6.3" x 3.0" | 9lbs
Additional Specifications available on separate datasheet
System Diagram
Target Vehicle
Scoring Sensor
(DSQ-50)
Telemetry Signal
Radar Signal
Projectile
Scoring Ground System
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
64
© 2010 Micro Systems, Inc
Specifications subject to change without notice
TEST SETS
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Micro Systems, Inc offers a variety of custom designed test sets for specialized applications. Our test
sets are available for laboratory, semi-controlled (i.e. hangar), and flightline/outdoor environments.
Available configurations include hand-held, rack mount, and ruggedized (MIL-T-28800). Our test set
capabilities range from Go/No-Go to comprehensive LRU testers, to complete target vehicle checkout
systems.
65
66
M41
Data Sheet
AS9100 Rev. C and ISO 9001-2008 Certified
Model 41 C-Band Test Set
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Full Bench top testing or quick Go/
No-Go testing options
Automated and Manual Tests
Radiate and Direct connect
operation Interface
Rugged and Portable design
Easy to use and highly configurable
to support multiple testing
Stores all test data for future
analysis and comparison
Removable Hard Drive
Applications
Bench Test C-Band Transponders
“Go/No-Go” Test C-Band
Transponders
Description
The Model 41 test set is a stand-alone unit that performs automated and manual bench and gono/go tests on compatible 5, 20, 50, and 400-Watt C-band Transponders. It is available in a rugged
shock-mounted transit case for field use and can also be removed from the case and installed in an
E.I.A. standard 19” equipment rack for lab or flight line use.
The Model 41 performs a full suite of transponder tests ideal for preflight equipment validation
and verification. It can be configured for a variety of frequency and pulse parameters to verify
Receiver Frequency, Receiver Sensitivity, Double Pulse Code Spacing, Transmitter Frequency,
Transmitter Pulse Width, Transmitter Output Power, and Relay Delay. The test set has an easy to
use Windows 7 based software application will all parameters and test panels controlled via touch
screen monitor. All test results are stored in a user defined directory and can be viewed either on the
test set or copied to a external device via the front panel USB interface.
The Model 41 can be operated in either Direct Mode with a supplied RF cable connecting the
transponder directly to the test set or in Radiate Mode with a supplied antenna to transmit and
receive signal to and from the transponder. It can support radiated Radiate Mode tests at distances
up to 50 feet.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
67
Technical Specifications
AS9100 Rev. C and ISO 9001-2008 Certified
Transmitter
Frequency:
Frequency Adjustment:
Frequency Stability:
Pulse Width:
Power Output Direct:
Power Output Radiate:
PGRF:
Pulse Code Spacing:
Operation Modes:
5.4 GHz to 5.9 GHz
1.0 MHz steps
+/- 2 MHz
Single Pulse: 0.5 sec +/- 0.2 sec
Double Pulse: 0.5 sec +/- 0.1 sec
0 dBm to <-70 dBm calibrated output to test Transponder receiver sensitivity
(adjustable in 1 dB steps)
> 30 dBm
1000 Hz (fixed)
3 sec to 15 sec in 0.1 sec steps
Radiate and Direct
Receiver
Frequency:
Frequency Adjustment:
RF Bandwidth:
Measurement Accuracy:
5.4 GHz to 5.9 GHz
1.0 MHz steps
5.35 GHz to 5.95 GHz
+/- 2 MHz
Environmental
Temperature:
Operating: -20 C to +65 C
Storage: -40 C to +70 C
Power Requirements
Input Voltage:
115 +/- 5 VAC, 60 Hz Single Phase
Functional Tests
Receiver Sensitivity
Receiver Frequency
Double Pulse Code Spacing
Transmitter Frequency
Transmitter Pulse Width
Transmitter Output Power
Reply Delay
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
68
© 2010 Micro Systems, Inc
Specifications subject to change without notice
M38-4
Data Sheet
AS9100C and ISO 9001:2008 Certified
Model 38-4 C-Band Mini Tester
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Small handheld device
PC Programmable Transmit
Frequency
Includes Antenna, Rechargeable
Battery, and Charger
Applications
“Go/No-Go” Test C-Band
Transponders
Description
The Micro Systems, Inc. C-Band Mini-Tester (Model 38-4) is a handheld battery powered unit that
provides go/no-go testing for the Micro Systems Models 251, 252, and 253 C-Band transponders and
the C-Band transponders produced by Herley Lancaster.
The Mini-Tester functions to verify proper transponder operation by interrogating a transponder
installed and powered in a systems platform. It is capable of testing compatible transponders at
distances of up to 350 feet. Indicator lights verify the transmission of signals and the received reply.
The Mini-Tester is also available as part of a kit that includes Mini-Tester, power supply,
programming set, cables, and carry case.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Transmitter
Frequency:
Frequency Adjustment:
Frequency Stability:
Pulse Width:
Power Output:
PGRF:
Pulse Code Spacing:
5.4 GHz to 5.9 GHz
1.0 MHz steps
+/- 5 MHz
0.5 sec +/- 0.1 sec
> 3 Watts
500 Hz (fixed)
2 sec to 16 sec in 1.0 sec steps, or single pulse
Receiver
Frequency:
Frequency Adjustment:
5.4 GHz to 5.9 GHz
Continuous, manually tuned
Environmental
Operating: 0 C to +50 C
Storage: -20 C to +65 C
Temperature:
Power Requirements
Power Source:
Battery Life:
Internal rechargeable battery with separate plug-in charger
4 hours with 1 test per minute
Physical
Dimension:
Weight:
2.50" W x 1.45" T x 6.25" D (excluding knobs)
25 ounces
Options
Universal Charger for International Use (reference Model 38-4i)
Carrying Case
Programming Set for programming transmit frequency in the field
USB Programmer
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
© 2010 Micro Systems, Inc
Specifications subject to change without notice
MPVTS
Data Sheet
AS9100C and ISO 9001-2008 Certified
Multi-Platform Vehicle Test Set (MPVTS)
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Easy to use Graphical User Interface
Automated and Manual Testing
L-Band or UHF RF Communication
Operate in Direct or Radiate Mode
Analog and Discrete Input/Output
Hi-current I/O
Rugged Transportable Design
Applications
Pre-mission Vehicle Checkout
“Go/No-Go” & Bench Testing
LRU Troubleshooting
Description
The Multi-Platform Vehicle Test Set (MPVTS) is a self-contained portable equipment rack test
instrument for performing vehicle electrical system verification. MSI can develop a custom MPVTS
software application designed specifically to perform complete pre-mission verification of your
airborne, ground, or marine vehicle. The MPVTS is the first test set designed to be completely
vehicle platform independent.
The MPVTS is used to provide control and monitoring of the communication and input and/or
output (I/O) signals to and from various vehicle platforms. It can display vehicle telemetry and
system status while allowing the test operator to transmit vehicle commands in either direct link or
radiate mode. Radiate Mode is RF Communication for UHF or L-Band datalinks. An embedded RF
Power Meter can be used to measure signal strength of radiated datalink. Direct link uses Ethernet,
USB, RS-232, or RS-422. Multiple Analog and Relay I/O channels are available for monitoring and
providing stimulus to vehicle systems. The MPVTS can also provide power to vehicle systems for
testing and verification. An embedded Oscilloscope can be used to monitor any analog, discrete, or
power signals.
The MPVTS is a turn-key system can be used to perform full Go/No-Go vehicle verification in
either manual or automated test modes. All equipment is encased in a portable, ruggedized transit
case that is quick and easy to setup to support any mission requirements.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
71
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Electrical
Input Power - MPVTS uses two primary power sources; 1 for internal components and the second for vehicle power
MPVTS Input Power: 115VAC +/- 10 VAC, 60Hz, 15 Amps
MPVTS Vehicle Power Supply Input: 115VAC +/- 10 VAC, 60 Hz, 30 Amps
Vehicle Power
6 High Current Outputs: 0 – 36VDC, 10A
4 Low Current Outputs: 0 – 20 VDC, 5A
Analog I/O
34 Inputs: 0 – 40 VDC (4kohm nominal load)
10 Inputs: 0 – 20 VDC (4kohm nominal load)
6 Ouputs: -10 – 10 VDC
Relay Closures
9 Relay Closures: 8 Normally Open (NO), 1 Normally Closed (NC)
Serial Communication
RS-422: 5 wire, 115,200 baud, 8, N, 1
RS-232: 9 pin
RS-485: 2 wire ,19.2 baud, 8, Odd parity, 1
USB: 3 ports on front panel
Ethernet: TCP/IP
RF Modules
UHF
Frequencies: 380 – 400 MHz, 435 – 450 MHz, or 358 – 380 MHz
Bandwidth: 20 kHz and 25 kHz available
Channels: 16
L-Band GRDCS Ground Station Module
Frequency: 915 MHz
Bandwidth: 1 kHz
Channels: 1
Physical
Size: 8U, E.I.A. Rackmount Transit Case - 30"W x 30"D x 23"H
Weight: Less than 150lbs
Temperature: +5 deg C to +40 deg C
Reliability (MTBF): 1000hrs
Options
RF Modules
Interface Cables
Rack Configuration
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
© 2010 Micro Systems, Inc
Specifications subject to change without notice
72
Model 59
Data Sheet
AS9100 Rev. C and ISO 9001-2008 Certified
Model 59 Test Set
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Rugged completely sealed design
Windows user interface
Direct and Radiate mode operation
UHF 380-400MHz datalink
Digital and Analog signal interfaces
Ruggedized laptop controller
10Base100 Ethernet Interface
Applications
Vehicle checkout
Bench test
Go/No-Go test
Description
The Model 59 Target Test Set is a portable test instrument used for verification of MQM-107D/E
avionics subsystems prior to launch. It includes a ruggedized laptop control interface that provides a
modern Windows-based computer environment for ease of operator use. The Test Set is designed to
provide complete closed loop (telemetry and command) test capabilities for airborne systems. It
simulates and displays telemetry parameters of the MQM-107D/E providing a complete system
environment that allows for full test and checkout of the electrical subsystems at various technical
levels on the flight line.
The Model 59 Test Set interfaces to the MQM-107D/E via a UHF datalink through either a direct
connection to the target using an RF cable or in radiate mode using an antenna. The test set
displays all target telemetry and system status information while allowing the test operator to transmit
target commands and receive telemetry downlinks.
The Model 59 Test Set is ruggedized and the modules are completely sealed for use outside or in
a hangar environment where the target electrical checks and engine run tests are performed prior to
launch. The Model 59 is currently available configured to test the MQM-107D/E sub-scale aerial
target. Other configurations are available.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
73
Technical Specifications
AS9100 Rev. C and ISO 9001-2008 Certified
Transmitter
Frequency:
Channels:
Channel Bandwidth:
Occupied Bandwidth:
Modulation:
Burst Data Rate:
RF Power Output:
Maximum PRF:
380 MHz to 400 MHz (Other frequency bands are available)
16
25 kHz
20 kHz
GMSK
14.4 kbps
4 Watts
10 Hz
Receiver
Sensitivity:
Selectivity:
Spurious Rejection:
-100 dBm @ 1x10-4 BER
-60 dB @ 12.5 kHz
-70 dB
Available Inputs/Outputs
8 Type 1 Discrete Inputs: 28V/GND
4 Type 2 Discrete Inputs: 28V/Open
2 Type 3 Discrete Inputs: 12V/Open
4 Type 4 Discrete Inputs: Open/GND
14 Type 5 Discrete Inputs: GND/12V
9 Type 6 Discrete Inputs: GND/4V (TTL)
4 Type 1 Analog Inputs:
3 Type 2 Analog Inputs:
12 Type 3 Analog Inputs:
1 Type 4 Analog Inputs:
4 Type 5 Analog Inputs:
0 – 32V
0 - 5V
+/- 20V
+/- 1V
+/- 10V
10 Type 1 Discrete Outputs: Open/28V
1 Type 2 Discrete Outputs: Open/12V
1 Type 3 Discrete Outputs: GND/Open
4 Type 4 Discrete Outputs: GND/12V
14 Type 5 Discrete Inputs: GND/12V
9 Type 6 Discrete Inputs: GND/4V (TTL)
1 Type 1 Analog Output:
0 – 5V
Environmental
Temperature:
Operating: -10 C to +60 C
Storage: -51 C to +71 C
Power Requirements
Input Voltage:
115 +/- 10 VAC, 47 - 63 Hz Single Phase
Physical
Dimension:
Weight:
23" W x 18" H x 30" L (including lid)
approximately 150 pounds (2-man lift)
Options
Custom Vehicle Interfaces
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
74
© 2010 Micro Systems, Inc
Specifications subject to change without notice
915MHz DTS
Data Sheet
AS9100 Rev. C and ISO 9001-2008 Certified
915MHz Data Link Test Set (DTS)
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Rugged completely sealed design
Linux user interface
Direct and Radiate mode operation
915MHz datalink
Digital and Analog signal interfaces
Ruggedized laptop controller
10Base100 Ethernet Interface
Applications
Vehicle checkout
Bench test
Go/No-Go test
Description
The 915MHz Data Link Test Set (DTS) is a portable test instrument used for verification of Data
Link Subsystem Replacement (DLS-r), Army Ground Station Unit (GSU), and other 915MHz Gulf
Range Drone Control Systems (GRDCS) communications equipment in compliance with the GRDCS
Data Link Format Specification. It includes a ruggedized laptop control interface that provides a
modern Linux-based computer environment for ease of operator use and high reliability. The DTS is
designed to provide complete closed loop (telemetry and command) test capabilities. It simulates
and displays telemetry parameters of the Unit Under Test (UUT) providing a complete system
environment that allows for full test and checkout of the electrical subsystems.
The DTS interfaces to the DLS-r via a 915-MHz Radio Frequency (RF) datalink through either a
direct connection using an RF cable or in radiate mode using an antenna. The test set displays all
target telemetry and system status information while allowing the test operator to transmit
commands and receive telemetry.
The DTS is ruggedized for use outside or in a hangar/lab environment. Other configurations are
available.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
75
Technical Specifications
AS9100 Rev. C and ISO 9001-2008 Certified
General
Frequency:
Modulation:
Antenna Port:
Operating System:
Test Points:
915 MHz +/- 9.15 kHz
BPSK
TX/RX, 50 ohms type N connector, Maximum VSWR 1.5:1
Windows/Linux (dual boot)
Sync, Code A, Code B, FSEL, TX Gate, TX Code, PROGEN, and +28VDC
Transmitter
Frequency:
Transmitter Power:
PRF:
Modulation:
915 MHz +/- 9.15 kHz
0 to -100dBm (Direct), > 0dBm (Radiate)
1 to 20 Hz
BPSK
Receiver
Frequency:
Dynamic Range:
915 MHz +/- 9.15 kHz
+30 dBm to +60dBM (Direct), +5 to < -75 (Radiate)
Functional Tests
Receiver Sensitivity
Receiver Dynamic Range
Transmitter Power
Current Draw
Variable DC Voltage (22 – 32 VDC)
Multiple GRDCS Messages, Data Quality Verification
Automated or Manual Testing
Radiate Test and Range Monitoring
Frequency/Spectrum Monitoring with External Test Equipment
Environmental
Temperature:
Pressure:
Operating: 0 C to +40 C
Storage: -20 C to +60 C
Sea level to 4000ft MSL
Power Requirements
Input Voltage:
115 +/- 10 VAC, 47 - 63 Hz Single Phase
Physical
Dimension:
Weight:
19.9" x 22.5" x 36.5"
130 lbs (typical)
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
76
© 2010 Micro Systems, Inc
Specifications subject to change without notice
Multipath Simulator
Data Sheet
AS9100 Rev. C and ISO 9001-2008 Certified
Multipath Simulator
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Rugged design
Bench Top or Rack Mountable
Laboratory or Field Use
915 MHz
High Power Input Capability
Easy to use
Applications
Troubleshooting Multipath Issues
UAV’s, Aircraft, Moving Vehicles
Fixed Sites
Description
The multipath simulator is a portable rugged test set used to add multipath effects to RF signals
at 915 MHz The simulator can be used in its rugged case, or removed and placed in the user’s 19
inch rack system.
The simulator receives the transmitted signal and passes the desired signal to the receiving
equipment. It also adds a multipath signal that can be delayed, attenuated or phase shifted at various
rates to simulate motion. There is a port located on the front panel for the user to add cable in line if
greater delays are required.
The simulator is useful for diagnosing system issues caused by signal reflection and motion. It
allows multipath problems to be diagnosed and eliminated in a laboratory environment.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
77
Technical Specifications
AS9100 Rev. C and ISO 9001-2008 Certified
General
Frequency:
Input Power Level (Max):
Multipath Atten Stps:
Multipath Delay Steps:
Phase Shift Rate:
Connectors:
900 to 930 MHz
650 W Peak, 20% Duty Cycle (J2 UUT)
0 to 8 dB in 2 dB steps and 0 to 40 dB in 10 dB steps
0 to 8ns in 2ns steps, 0 to 40ns in 10ns steps and 100ns
0, 0.001, 0.1, 1.0, 10.0 and 100 seconds
Type N Female
Power Requirements
Input Voltage:
115 +/- 10VAC, 47 – 63 Hz Single Phase
Environmental
Temperature:
Operating: 0 C to +50 C
Storage: -20 C to +60 C
Physical
Dimension (Transit Case): 11.1" H x 22.5" W x 36.5" L (including lid)
Dimension (Drawer):
19" rack mountable, 3U, 23.5" Deep
Weight:
approximately 150 pounds (2-man lift)
Options
Custom Vehicle Interfaces
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
78
© 2010 Micro Systems, Inc
Specifications subject to change without notice
FLIGHT TERMINATION
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Micro Systems, Inc is a leading global provider of turn-key solutions for a full range Flight Termination
Systems (FTS) and ancillary devices. Our product line includes; Portable Flight Termination Systems,
Dual Redundant 200 Watt to 1.5kW FTS, Receiver/Decoder FTS Test Sets, IRIG Tone Generators/
Exciters, Command Sequencers, Auto Switchover Units, and FTS Receiver Monitors. Additionally, our
multi-rack range integrated Flight Termination Systems are fully modular in design to allow system
flexibility and upgradeability. We utilize the latest suite of Graphical User Interface (GUI) software
applications to provide ease of use and operation. All of our products can be customized to meet your
specific requirements. In addition, we can also offer full system integration and training to ensure quick
easy implementation.
79
80
Flight Termination
System
AS9100C and ISO 9001:2008 Certified
Flight Termination System
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
IRIG 319 compliant command
signals
Redundant transmitters
Fault Detection
Ethernet interface for remote
control, monitoring and antenna
positioning data
Data recording and time stamping
Command tone verification
Automatic 1:1 redundancy
Field serviceable and upgradeable
Applications
Provide Flight Termination for airborne
platforms for safe, reliable, range safety
applications.
Description
The Micro Systems, Inc. Flight Termination System (FTS)is a turn-key system capable of
transmitting MONITOR, ARM, and TERMINATE flight termination encoded command signals as well
as the 20 individual IRIG tones up to 6 simultaneously. The system can be manually or automatically
switched between transmitters, includes fault monitoring, audio alarms, data recording and system
time stamping, and full remote control operation and configuration. The system is ready for
installation in E.I.A. 19 inch standard racks for mobile platforms or in transportable cases high
portability.
The redundant transmitter system generates a 1000W Wideband FM signal that can be routed to
two pedestal antennas for full redundant operation. FTS commands are initiated either at the
Command Control Unit (CCU) front panel when in Local Mode or from the remotely located Master
Control Module via Ethernet link when in Remote Mode. The initiated command signals are IRIG319 compliant and compatible with the Herley Industries HFTR60 (or compatible) Flight Termination
Receivers (FTR).
The FTS also includes a command verification Receiver Monitor Unit (RMU) complete with Omniantenna kit for monitoring transmitted commands from a remote location. The RMU interfaces to the
FTS via Ethernet link for data recording and time stamping capability.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by81
the International Trade in Arms Regulations (ITAR)
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Command Control Unit
Carrier Frequency:
406 MHz to 450 MHz, adjustable in 100 kHz steps, +/- .005% Tolerance
FTS Commands:
MONITOR, ARM, TERMINATE
IRIG Tone Frequencies:
1 – 20 (up to 6 on simultaneously), Tolerance +/-0.1
Exciter Output Power:
0 dBm
Modulation:
Wideband FM
Interface:
Ethernet
Prime Power:
Universal AC - 115 to 230 VAC, 50-60 Hz
Equipment Enclosure:
Standard 19 inch transit case with Front and Rear covers and shock mounted internal frame
Feature Enhancements:
Data Recording/Event Time Stamp, Fault Detection, Audio Alarm, Manual/Auto Switchover
Indicators:
Illuminated LED’s
1000W RF Power Amplifier Module
Frequency Range:
400 MHz to 450 MHz
Output Power:
1000 Watts (typical)
Power Input:
0 dBm
Prime Power:
180 to 260 VAC, single phase
Equipment Enclosure:
E.I.A. Standard 19", 5U High, 22" deep, 80lbs
Display:
Fwd/Rev Power, Gain Adjustment, ALC Fast/Slow, On/Off, Fault Indication, Standby Mode
Interface:
Ethernet
Receiver Monitor Unit
Frequency Band:
406 MHz to 450 MHz, adjustable in 100 kHz steps
Sensitivity:
-107 dBm
Response Time:
15ms nominal
Prime Power:
115 to 230 VAC, 50-60 Hz
Equipment Enclosure:
Standard 19 inch transit case with Front and Rear covers and shock mounted internal frame
System Includes:
2 Command Control Units
2 High Power RF Amplifiers
1 System Failover Controller
1 Master Control Console
Associated cabling
1 Receiver Monitor Unit w/ associated
antenna kit
Ethernet Switch
Operation Manual
Training
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
82
© 2010 Micro Systems, Inc
Specifications subject to change without notice
FTS-200W
Data Sheet
AS9100C and ISO 9001-2008 Certified
Flight Termination System – 200W Dual Vehicle
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
EIA 19" Rack Components
Independent Control of up to 2
vehicles
RF Power Output of 200 Watts
IRIG 313-01 Compliant
MONITOR, ARM and DESTRUCT
Command Switches
Safety wire switch protection caps
Universal AC input power
Applications
Range Safety
Test
Description
The Micro Systems Inc. 200W Dual Vehicle FTS was specifically designed for use with
Unmanned Aerial Vehicles (UAV’s), missile systems and aerial target drones and is currently in
operation supporting various missions worldwide.
Designed to be IRIG 313-01 and 319-07
compliant, it is a rack mount unit used for flight termination and command. The unit accepts AC
power and generates a modulated RF output FM signal suitable for interrogation of flight termination
receivers such as the Herley HFTR60 and a variety of command receiver/decoders.
The 200W Dual Vehicle FTS features two sets of command switches on the front panel for
MONITOR, ARM, and DESTRUCT to provide quick and easy emergency control of up to two
vehicles in flight. All command switches have protective switch covers to prevent unintentional
command initiation A battery backup module capable of providing back up power for up to 15
minutes can also be added to the system. From the control panel the operator can monitor
command status indicator lamps and there is also a panel meter for monitoring AC input power.
The 200W Dual Vehicle FTS internally generates command tones that modulate the synthesized
RF carrier to produce a 200 Watt (minimum) RF output. Upon power up, the system will immediately
transmit the carrier frequency and will continue to do so until the DESTRUCT command is issued.
The MONITOR and ARM switches can be toggled ON/OFF independently of each other to send the
corresponding command tone combinations listed on page 2 of this datasheet. To initialize the
DESTRUCT command the ARM command must first be initialized.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
83
Technical Specifications
AS9100C and ISO 9001-2008 Certified
Specifications
Transmitter System
Power Input:
Carrier Frequency:
Tone Frequencies:
Carrier Frequency Stability:
Power Output:
Output Impedance:
Output Connection:
Modulation:
Spurious Outputs:
Vehicle 1 Commands:
Vehicle 2 Commands:
Protection:
Enclosure:
Dimensions:
Weight:
Universal Input: 115 VAC to 230 VAC, 50 to 60 Hz
User Adjustable between 406 – 450 MHz in 100 kHz steps
1, 2, 3, 5, 6 and 7 per IRIG 313-01
±.0005%
200 Watts (nominal)
50 ohms
Type N Female
Wideband FM, ±30 kHz per tone
-50 dBc
MONITOR – Apply Tone 5 (12.14 kHz)
ARM – Apply Tone 1 (7.50 kHz) to Tone 5
DESTRUCT – Remove Tone 5, Add Tone 2 (8.46 kHz) to Tone 1
MONITOR – Apply Tone 6 (13.70 kHz)
ARM – Apply Tone 3 (9.54 kHz) to Tone 6
DESTRUCT – Remove Tone 6, Add Tone 7 (15.45 kHz) to Tone 3
RF Output protection
Circuit Breaker/Fuse protected
EIA 19" Shockmount case
28.5 x 22.5 x 21.6 inches
Less than 120 lbs
Receiver System
Power Input:
Carrier Frequency:
Tone Frequencies:
Sensitivity:
Maximum Input Power:
Vehicle 1 Commands:
Vehicle 2 Commands:
Protection:
Enclosure:
Dimensions:
Weight:
Universal Input: 115 VAC to 230 VAC, 50 to 60 Hz
User Adjustable between 406 – 450 MHz in 100 kHz steps
1, 2, 3, 5, 6 and 7 per IRIG 313-01
-106 to -115 dBm
+13 dBm
MONITOR – Apply Tone 5 (12.14 kHz)
ARM – Apply Tone 1 (7.50 kHz) to Tone 5
DESTRUCT – Remove Tone 5, Add Tone 2 (8.46 kHz) to Tone 1
MONITOR – Apply Tone 6 (13.70 kHz)
ARM – Apply Tone 3 (9.54 kHz) to Tone 6
DESTRUCT – Remove Tone 6, Add Tone 7 (15.45 kHz) to Tone 3
RF Output protection
Circuit Breaker/Fuse protected
EIA 19" Shockmount case
24 x 22.5 x 9.3 inches
Less than 50 lbs
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
84
© 2010 Micro Systems, Inc
Specifications subject to change without notice
FTS - Transportable
Data Sheet
AS9100C and ISO 9001:2008 Certified
Transportable Flight Termination System (FTS)
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Primary and Redundant
Transmit Antennas
Receive Antenna
Command Control Unit
Power Amplifier Module
Receiver Monitor Unit
Airborne Flight Termination
Receiver (FTR)
The Micro Systems Flight Termination System (FTS) is a
complete turn-key system that includes a Command Control Unit,
High Power RF Amplifiers, Receiver Monitor Unit, Antenna Kits
and airborne Flight Termination Receiver (FTR). It is a redundant
self-contained, portable 425 MHz system that transmits IRIG 31301 compliant commands to Monitor, Arm, and Destruct a vehicle in
flight. FAULT monitoring and an auto switch-over from Primary to
Redundant components are standard features that make the FTS
a safe and reliable range safety system.
Features
Transmit Power Options Available
IRIG 313-01 Compliant
Redundant RF Power Amplifiers
Automatic 1:1 Redundancy
Fault Detection
Primary and Redundant Modes of
Operation
Remote Control (optional)
Command Tone Verification
Multi-Vehicle Control (optional)
Ruggedized Design
The FTS is a transportable modular design that is highly
maintainable and easily upgraded for future applications. The
system is set up in seconds and ready for deployment in
ruggedized shock-mounted cases. The Command Control Unit
(CCU) contains the solid-state encoder/exciter that generates the
RF command messages when the control switches on the front panel are initiated. The RF command messages are
output from the CCU to the RF Power Amplifier Module where they are amplified and transmitted. The transmitted
signal is received and processed by the Flight Termination Receiver in the airborne vehicle. The transmitted signal is
also received and can be monitored on the ground using the remote Receiver Monitor Unit (RMU). The FTS is a
advanced high reliable and safe system to handle all of your range safety requirements.
The FTS is a robust design with many options available for a system that meets the exact needs of our customers.
FTS Commands, multi-vehicle control tone assignments, RF power level, antenna configuration, and remote control
capabilities are all configurable parameters that can be specified at time of order. Additionally, Micro System can
provide full system integration and training at our customer’s on-site location.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
85
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Command Control Unit
Carrier Frequency:
406 MHz to 450 MHz, adjustable in 100 kHz steps
Carrier Frequency Tolerance:
+/- .0005%
Tone Frequencies:
Tone 1: 7.5 kHz | Tone 2: 8.460 kHz | Tone 5: 12.14 kHz | Tone 7: 15.450 kHz - additional tones avilable
Tone Frequency Tolerance:
+/-0.1
RF Output Power:
50 Watts (minimum at output)
Modulation:
Wideband FM
Multi-Vehicle Control:
Up to 2 vehicles simultaneously
Prime Power:
115 to 230 VAC, 50-60 Hz
Equipment Enclosure:
Standard 19 inch transit case with Front and Rear covers and shock mounted internal frame
Fault Detection:
RF Output Power, Tone Monitor
200W RF Power Amplifier Module
Frequency Range:
400 MHz to 450 MHz
Saturated Output Power:
200 Watts (typical) - Additional options available
Power Input:
50 Watts
Prime Power:
115 to 230 VAC, 50-60 Hz
Equipment Enclosure:
Standard 19 inch transit case with Front and Rear covers and shock mounted internal frame
Receiver Monitor Unit
Frequency Band:
406 MHz to 450 MHz, adjustable in 100 kHz steps
Sensitivity:
-107 dBm
Response Time:
15ms nominal
Prime Power:
115 to 230 VAC, 50-60 Hz
Equipment Enclosure:
Standard 19 inch transit case with Front and Rear covers and shock mounted internal frame
Antenna Kit
Antenna:
Directional, circular polarized
Mounting:
Tripod, Tower, or Mast options available
Cables:
RG-214 included
Flight Termination Receiver – Separate datasheet
System Diagram
Flight Termination Receiver
(FTR)
Airborne Vehicle
FTS Transmitter System
Remote FTS Receiver
System
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
86
© 2010 Micro Systems, Inc
Specifications subject to change without notice
FTS - Portable
Data Sheet
AS9100C and ISO 9001:2008 Certified
Portable Flight Termination System
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Includes: Command Control Unit,
Remote Monitor Unit, Remote
Control Unit
IRIG 313-01 Compliant
Redundant RF Power Amplifiers
Automatic 1:1 Redundancy
Fault Detection
Primary and Redundant Modes of
Operation
Remote Control
Command Tone Verification
Ruggedized Design
Applications
Range Safety
15, 25, and 50 Watt RF transmitter
configurations available (contact us
for custom requirements)
Description
The Micro Systems, Inc Flight Termination System (FTS) is a redundant self-contained, portable
425 MHz wideband FM system that can transmit the necessary codes to Monitor, Arm, and Destroy a
missile in flight.
The FTS consists of a Transmitter Systems and a Receiver System. The Command Control Unit
(CCU) is the Transmitter System used for encoding IRIG flight termination commands. The Remote
Monitor Unit (RMU) is the Receiver System for detecting, decoding, and monitoring commanded
signals from the CCU. A Remote Control Unit (RCU) is also included for initiating FTS commands
remotely from the CCU.
The FTS is currently available with CCU transmitter configurations for 15 Watt, 25 Watt, and 50
Watt RF Output Power.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
87
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Electrical
Carrier Frequency:
Carrier Frequency Tolerance:
Tone Frequencies:
Tone Frequency Tolerance:
RF Output Power:
Modulation:
425 MHz
+/- .0005%
Tone 1
7.50 kHz
Tone 2
8.46 kHz
Tone 4
10.76 kHz
Tone 5
12.14 kHz
+/- 0.1
15 Watts, 25 Watts, or 50 Watts
Wideband FM
Operational
Tone Sequences:
Time Between Commands:
Fault Detection:
MONITOR – Apply Tone 5
ARM – Add Tone 1 to Tone 5
DESTRUCT – Remove Tone 5 and add Tone 2 to Tone 1
500 ms
RF Output Power
Transmit Tone ≠ Monitored Tone
Power Requirements
Input Voltage:
Available for DC input voltage or AC input voltage applications
Mechanical
Equipment Enclosure:
Cooling:
Aluminum Zero Case
Fans mounted directly to RF power amplifers
Options
Antenna
RF Power Meters
RF Power Levels
Input Voltage
Command Tone Configurations
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
88
© 2010 Micro Systems, Inc
Specifications subject to change without notice
FTTS-P-8
Data Sheet
AS9100C and ISO 9001:2008 Certified
Flight Termination Test Set – 8 Tone
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
Portable
8 Tones (1 - 8 standard)
IRIG 313-01 Compliant
Variable RF Output Level
Variable Carrier Frequency
20 Tone model also available
Antenna and Coaxial Cable included
Applications
Range Safety
Test
Description
The Micro Systems, Inc. Model FTTS-P-8 Flight Termination Test Set (FTTS) is a portable unit
used for flight-line checkout of flight termination receivers and/or command receiver/decoders.
The FTTS accepts AC power and generates a modulated RF output suitable for interrogation of
flight termination receivers and/or command receiver/decoders.
The FTTS can transmit up to 6 tones simultaneously and the RF output power is adjustable from
0 to -127 dBm. The IRIG tones can be switched ON/OFF independently from the control panel.
A 20 Tone version of the FTTS is also available
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
89
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Specifications
Size:
Weight:
Power Input:
Carrier Frequency:
Carrier Frequency Stability:
Power Output:
Output Impedance:
Output Connection:
Modulation:
Tone Frequencies:
Remote Control:
Spurious Outputs:
Harmonic Distribution:
9.00” H x 12” W x 5" D (Standard EIA 19” Rack Mount)
approximately 10 pounds
Universal Input: 115 VAC to 230 VAC, 50 to 60 Hz
405 to 450 MHz in 100 kHz steps
±.0005%
0 to -127 dBm
50 ohms
Type N Female
Wideband FM, ±30 kHz per tone
Any combination of up to 8 tones per IRIG 313-01
(maximum of 6 tones ON simultaneously)
RS-232 (other options available)
-50 dBc
< 2%
Options
Rackmount
Select any 8 of 20 available Tones
20 Tone model available (FTTS-P-20)
Local/Remote: RS-232, GPIB, or 10Base100 Ethernet
Customizable to fit your needs
20 Tone Model
(FTTS-P-20)
Ready for
Transport
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
90
© 2010 Micro Systems, Inc
Specifications subject to change without notice
CEE-8-I
Data Sheet
AS9100C and ISO 9001:2008 Certified
Command Encoder/Exciter – 8 Tone
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
EIA 19" Standard Rackmount
8 Tones (1 - 8 standard)
IRIG 313-01 Compliant
Variable RF Output Level
Variable Carrier Frequency
Carrier ON/OFF Switch
Local and Remote Control
20 Tone model also available
Applications
Range Safety
Test
Description
The Micro Systems, Inc. Model CEE-8-I Command Encoder/Exciter (CEE) is a rack mount unit
used for Flight Termination Systems for checkout of flight termination receivers and/or command
receiver/decoders.
The CEE accepts AC power and generates a modulated RF output suitable for interrogation of
flight termination receivers and/or command receiver/decoders.
The CEE can transmit up to 6 tones simultaneously and the RF output power is adjustable from 0
to -127 dBm. The IRIG tones can be switched ON/OFF independently from the control panel. The
CEE can be controlled in Local mode using the front panel switches or in Remote mode using an RS232 or GPIB interface.
A 20 Tone version of the CEE is also available
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
91
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Specifications
Size:
Power Input:
Carrier Frequency:
Carrier Frequency Stability:
RF Power Output:
Output Impedance:
Output Connection:
Modulation:
Tone Frequencies:
Remote Control:
Spurious Outputs:
Harmonic Distribution:
3.50” H x 18.75” D (Standard EIA 19” Rack Mount)
Universal Input: 115 VAC to 230 VAC, 50 to 60 Hz
406 to 450 MHz in 100 kHz steps
±.0005%
0 to -127 dBm
50 ohms
Type N Female
Wideband FM, ±30 kHz per tone
Any combination of up to 8 tones per IRIG 313-01
(maximum of 6 tones ON simultaneously)
RS-232 (other options available)
-50 dBc
< 2%
Options
Portable
Select any 8 of 20 available Tones
20 Tone model available
Local/Remote: RS-232, GPIB, or 10Base100 Ethernet
Customizable to fit your needs
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
92
© 2010 Micro Systems, Inc
Specifications subject to change without notice
CEE-20-R
Data Sheet
AS9100C and ISO 9001:2008 Certified
Command Encoder/Exciter – 20 Tone
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
EIA 19" Standard Rackmount
20 Tones
IRIG 313-01 Compliant
Variable RF Output Level
Variable Carrier Frequency
Carrier ON/OFF Switch
Local and Remote Control
8 Tone model also available
Applications
Range Safety
Test
Description
The Micro Systems, Inc. Model CEE-20-R Command Encoder/Exciter (CEE) is a rack mount unit
used for Flight Termination Systems and for checkout of flight termination receivers and command
receiver/decoders.
The CEE accepts AC power and generates a modulated RF output suitable for interrogation of
flight termination receivers and/or command receiver/decoders.
The CEE can transmit up to 6 tones simultaneously and the RF output power is adjustable from 0
to -127 dBm. The IRIG tones can be switched on or off independently from the control panel. The
CEE can be controlled in Local mode using the front panel switches or in Remote mode using an RS232 or GPIB interface.
An 8 Tone version of the CEE is also available
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Specifications
Size:
Carrier Frequency:
Carrier Frequency Stability:
Power Output:
Output Impedance:
Output Connection:
Modulation:
Tone Frequencies:
Remote Control:
Spurious Outputs:
Harmonic Distribution:
3.50” H x 18.75” D (Standard EIA 19” Rack Mount)
406 to 450 MHz in 100 kHz steps
±.0005%
0 to -127 dBm
50 ohms
Type N Female
Wideband FM, ±30 kHz per tone
20 tones per IRIG 313-01
(maximum of 6 tones ON simultaneously)
RS-232 (other options available)
-50 dBc
< 2%
Options
Portable
8 Tone model available
Local/Remote: RS-232, GPIB, or 10Base100 Ethernet
Customizable to fit your needs
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
© 2010 Micro Systems, Inc
Specifications subject to change without notice
CEE-3-XRXA5W
Data Sheet
AS9100C and ISO 9001:2008 Certified
Command Encoder/Exciter – 5 Watt
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
EIA 19" Standard Rackmount
Individual Tone Control: 1, 2, 5
(standard)
IRIG 313-01 Compliant
RF Output Power of 5 Watts (other
options available)
Carrier ON/OFF Switch
Adjustable Carrier Frequency
Applications
Range Safety
Test
Description
The Micro Systems Inc. Model CEE-XRXA5W was specifically designed for use with Unmanned
Aerial Vehicles (UAV’s), missile systems and aerial target drones and is currently in operation
supporting various missions worldwide. Designed to be IRIG 313-01 and 319-07 compliant, it is a
rack mount unit used for flight termination and command. The unit accepts AC power and generates
a modulated RF output FM signal suitable for interrogation of flight termination receivers such as the
Herley HFTR60 and a variety of command receiver/decoders.
The basic CEE-XRXA5W features a three tone switches on the front panel that can be factory set
to the frequencies of your choice. The unit also features thumbwheels switches for setting the carrier
frequency from 406 MHz to 450 MHz in 100 kHz steps as well as a carrier ON/OFF switch.
Internally generated command tones modulate the synthesized RF carrier to produce a 5 Watt
(minimum) RF output. Upon power up, the CEE-XRXA5W will immediately transmit the FM carrier
frequency and the three tone switches can be turned ON/OFF independently to allow the operator to
output any command tone sequence. There are many different variations of the unit available.
Individual tone selection, FTS command tone sequences, switch configuration, RF output power, and
many other options are available to meet any mission requirement.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Specifications
Power Input:
Carrier Frequency:
Tone Frequencies:
Carrier Frequency Stability:
Power Output:
Output Impedance:
Output Connection:
Modulation:
Spurious Outputs:
Commands (Optional):
Universal Input: 115 VAC to 230 VAC, 50 to 60 Hz
406 to 450 MHz in 100 kHz steps
1 through 20 are available per IRIG 313-01
±.0005%
5 Watts (minimum) and higher power options are available
50 ohms
Type N Female
Wideband FM, ±30 kHz per tone
-50 dBc
MONITOR – Tone 5
OPTIONAL – Tone 4
ARM – Tone 5 + Tone 2
DESTRUCT – Tone 2 + Tone 1 minus Tone 5
Size:
Weight:
5.25” H x 18.75” D (Standard 3U EIA 19” Rack Mount)
Less than 20lbs
Options
Portable
Tone Assignments
RF Power Level
FTS Commands
Local/Remote: RS-232, GPIB
Permanently attached power cord
Customizable to fit your needs
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
© 2010 Micro Systems, Inc
Specifications subject to change without notice
TRD-20
Data Sheet
AS9100C and ISO 9001:2008 Certified
Tone Receiver/Decoder – 20 Tone
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
Features
EIA 19" Standard Rackmount
20 Tones
IRIG 313-01 Compliant
Signal Strength Display Meter
Variable Carrier Frequency
Local and Remote Control
Applications
Range Safety
Test
Description
The Micro Systems, Inc. Model TRD-20 Tone Receiver/Decoder (TRD) is a rack mount RF
receiver that will display the presence of any of the 20 individual tones or combination command
tones.
The unit was designed to conform with the requirements set forth in the IRIG Standard 313-01 of
the Range Commanders Council (RCC) and to detect and display up to 6 tones simultaneously.
The rear panel connections include RF IN, Signal Strength, and Decoded Channel outputs of the
20 tone detector circuits.
Export Sales of this product are subject to U.S. Government approval.
Sales will not be approved to countries prohibited by the International Trade in Arms Regulations (ITAR)
97
Technical Specifications
AS9100C and ISO 9001:2008 Certified
Specifications
Size:
Power Input:
Carrier Detect:
Channel Deviation Threshold:
Channel Bandwidth:
RF Input:
RF Sensitivity:
Decoded Channel Output:
Remote Control:
Signal Strength:
3.50” H x 18.75” D (Standard EIA 19” Rack Mount)
Universal Input: 115 VAC to 230 VAC, 50 to 60 Hz
Front Panel LED display and discrete output on rear panel
± 10 to ± 15 kHz
± 1% Minimum @ 2 dB Bandwidth
± 4% Maximum @ 14 dB Bandwidth
406 MHz to 450 MHz, 50 ohm BNC female connector
- 100 dBm
DB-37 Female output connector driven by an Open Collector, DC output
module
RS-232 (other options available)
Voltage ranges from 0 VDC to 5 VDC
Options
Portable
IF Input
Audio Input
Compact hard case for portable use
Local/Remote: RS-232, GPIB, or 10Base100 Ethernet
Decoded Channel Output – TTL Logic or Contact Closures
Customizable to fit your needs
Contact us for custom modifications
For additional information contact:
Micro Systems, Inc.
35 Hill Ave
Fort Walton Beach, FL 32547
PH: 1-888-325-9422
FAX: 1-850-243-1378
www.gomicrosystems.com
98
© 2010 Micro Systems, Inc
Specifications subject to change without notice
CONDITIONS OF SALE
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
99
CONDITIONS OF SALE
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
100
CONDITIONS OF SALE
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
101
CONDITIONS OF SALE
35 Hill Ave Fort Walton Beach FL 32548 | PH: 1-888-325-9422 | Fax: 1-850-243-1378 | www.gomicrosystems.com
102
Providing High Performance Command & Control,
Flight Termination and Range Safety Systems
Since 1976
35 Hill Ave
Fort Walton Beach, FL 32548
PH: 1-888-324-9555
FAX: 1-850-243-1378
marketing@gomicrosystems.com
www.gomicrosystems.com