Oles Honchar Dnipropetrovsk National University
International Programm
PHYSICAL AND TECHNICAL FACULTY
Dean, Professor. O M Petrenko
Departments
e-mail: kpk.ftf@dnu.dp.ua
Tel.: + 38 056 3731258
Department of Design and construction
Department of Technology
Department of Engines
Department of automatic control systems
Department of electronic automation
Department of Robotic Systems
Department of Engineering Mechanics
Department of Life Safety
Contact
Dean of International Cooperation, PhD
TV Labutkina
e-mail: serg_davydov@mail.ru
Tel.: + 38 099 3814819
SPECIALITY “ROCET AND SPACE SYSTEMS”
MASTER
Educational and professional programs designed to meet the latest advances in rocketry,
mathematical methods, information technology, space programs trends for different purposes, and
related manufacturing processes.
Educational and professional program designed to prepare professionals:
- Training areas "Aviation and Rocket";
- Educational level of "complete higher education";
- Specialty "missile and space systems";
- Master Program "Rocket and space complexes";
- Qualification of " Professional in the industry of mechanical engineering";
One year of study (60 credits) provides a theoretical and practical training in basic and
specialized courses in the field of rocketry. The highly qualified staff of teachers (doctors, professors,
PhD) teaches courses up to date using the latest international scientific achievements. The student may
select a set of courses, but keep in mind the need to have some basic knowledge to learn the course
successfully.
As an example of selecting courses totaling 60 credits may be as follow:
1
№
1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
№ general list of courses
Discipline
Calculation of the strength RS aircrafts
Launch Vehicle Production
Design SC SR (a small range)
Designing of power systems of aircraft
Design of onboard hardware system
Design of boosters and spacecraft
Effectiveness SC
Design spacecraft
Sheet and volume stamping technique summary
Liquid Rocket Engines Production Engineering
Summary
Total
7
2
7
4
11
4
7
7
5
6
60
THE TOTAL LIST OF DISCIPLINES
credits
№
1
1
2
3
Discipline
2
Calculation of
the strength RS
aircrafts
Launch
Vehicle
Production
Design SC SR
Brief description of the discipline
(ECTS)
Semester
/year
3
4
5
7,0
1/2014
2,0
1/2014
7,0
1/2014
Subject and objectives of the course. Methods for
calculating RS aircrafts structures made of composite
materials : characteristics of physical and mechanical
properties of the composite materials , the ratio of
elasticity for composite materials, single-layer
design, three-layer structure ( with a solid filler and
mass-strength with honeycomb ) , beams , frames and
trusses with КM , optimization of design parameters.
Calculation of shells of revolution with KM, the
choice of the optimal parameters of reinforcement.
Features load power RS aircrafts structural elements
with dynamic operations in space, types of
oscillations , transients , formation of the dynamic
characteristics of the spacecraft .
Main characteristics and structure design basis of
Launch
Vehicle Production Engineering techniques and
hardware for the production of
- dry compartments
- propellant compartments
- propulsions
Aerodynamic classification schemes and aircraft.
Classification of aircraft, special purpose, their
features. Organization design. Design stage. Features
various aerodynamic schemes and methods of their
choice. Features of SR aircraft. Geometric, weights
and other parameters that must be considered in the
design. The choice of geometric parameters of the
wings. Determination of geometric parameters of the
2
1
4
5
6
7
8
2
3
case. Aeroupruhist. Flater. Baftinh. Features external
forms of hypersonic aircraft.
General information about the power system.
Designing
power systems of Fuel tanks. Purpose of the basic requirements, the
design problem. Calculate the volume of fuel and its
aircraft
dynamics in the tanks of aircraft design parameters
boost fuel tanks, aircraft fence devices, piping.
Choosing general design parameters of power
aircraft.
Available techniques or choose conditions for
Design
selection of basic parameters on-board systems of
onboard
hardware system automatic space vehicles (SV). We present the basics
of design of individual nodes SV. Specific features of
the development of leaky sections of the apparatus.
Much attention is paid to the relationship between the
parameters of individual systems, flight path,
program design and flight SV. There have been
claims that are proposed for construction of the SVside developers onboard systems.
General methodology design. Functional and
Design booster
structural
composition of the spacecraft . Materials
and spacecraft
used in the construction of spacecraft . Build an
airtight container and its components. Frame design
for placing devices in an airtight container. Means for
attaching devices to the frame. Frames for placing
devices on the outer surface hermokonteyneru .
Typical design mounts spacecraft . Electrical
interfaces with the spacecraft launch vehicle . The
design of the spacecraft with tight cover.
Constructions of space platforms. Construction of
solar panels . Constructive fastening base station to
the spacecraft . Means of transmission to
hermokonteyneru ( current collectors ). The design of
passive and active thermal control of spacecraft . The
design elements of zachekovky . Features of the
operation and design of devices that turn structures
spacecraft . Construction elements of life support
systems . Construction elements Lander . Structural
and layout schemes upper stage . Construction of fuel
tanks and spacecraft booster.
The aim of the course is to teach students to
Effectiveness
create
a body of knowledge and information about
SC
the methodology of analyzing the effectiveness of
complex engineering systems, including space-rocket
complexes.
The acquisition of technology, methods and means of
Design
designing spacecraft. Practical skills of designing
spacecraft
spacecraft. Analysis of space technology, the range of
problems faced by the specialist and possible
solutions, all necessary design calculations at all
stages of spacecraft.
3
4
5
4,0
2/2015
11,0
2/2015
4,0
1/2014
7,0
1/2014
7,0
2/2015
1
9
10
2
Sheet and
volume stamping
technique
Summary
Liquid Rocket
Engines
Production
Engineering
Summary
3
4
5
The theoretical and practical basis of sheet and
volume stamping for launch vehicle and spacecraft
parts production are studied. Such parts as
aerodynamic fairings, shells and bottoms of tanks,
engines and dry compartments, pipelines, structural
rings, bellows joint and other are considered.
5,0
1/2014
The theoretical and technological basis of liquid
rocket engines production engineering is studied.
Such parts as injection head, cooling jacket, pipelines
and other are considered.
6,0
2/2015
4