OMEGA PROJECT TEAM: ALPHA Members: Alexandra Salgado Shaun Besse Lizzabeth Ponce Expected Results Julich Ozone Sonde Intercomparison Experiment System Design • • • • • • • 1. 2. 3. 4. 5. 6. 7. Power supply system Data-processing system Electrical system Launch system Mechanical system Thermal system Ozone sensor system Power Budget Power Budget (cont.) Power Budget (cont.) Battery Specification www.energizer.com Battery Specifications (cont.) www.energizer.com Battery Specifications (cont.) www.energizer.com Data-Processing System The software: - 1. The uploading software Allows the user to download data from the EEPROM using a PC as the user interface . 2. The mission software Talks to the sensors. Electrical system Temp. Reader Ozone Sensor Multiplexer Enable On/Off Pressure Sensor Clock Signal Analog To Digital Converter 12 bit System Reset Heater On/Off Basic Stamp Processor Clock Signal Memory Memory input Real Time Clock Signal Real Time Clock Launch system Top View of Spacecraft interface * The interface to the spacecraft will consist of two metal tubes attached to two corners of the payload box. * The two corners will be opposite a diagonal. Mechanical Design Payload Box Dimensions 18.5 cm x 14.5 cm x 14.5 cm Ozone/Heater compartment Dimensions 16cm x 9cm x 9cm Mechanical Design (cont.) Electronic Compartment Battery compartment Thermal System A1: Area of conducting surfaces A2: Area of radiating surfaces Pc: Power that is being conducted out of the payload Pr: Power that is being radiated out of the payload σ: Boltzmann constant e: emissivity k: conductivity Ozone Sensor System Weight Budget 700 g from ACES program office 200 g from Team “JHK” 100 g from Team “Late Ballooners” Budget Main Schedule Activity Mission Objectives Project Management Payload Design Science Abstract and WBS Payload Development Plan Payload Construction Plan Master Budget Written PDR Preliminary Design Review Critical Design Review Ordering of Parts Fabrication of Payload Box Receiving ordered parts Build Ozone Sensor system Build Electrical system Test built systems Assemble payload Test assembled payload Flight Readiness Review (FRR) Launch Trip Start Mon 2/3/03 Finish Wed 2/5/03 Thu 2/6/03 Wed 2/5/03 Tue 2/11/03 Thu 2/13/03 Fri 2/14/03 Thu 2/13/03 Thu 2/13/03 Thu 2/13/03 Wed 2/19/03 Thu 2/27/03 Thu 4/10/03 Fri 4/11/03 Mon 4/14/03 Mon 4/20/03 Wed 4/23/03 Wed 4/23/03 Sat 4/26/03 Thu 5/1/03 Fri 5/2/03 Thu 5/8/03 Fri 2/14/03 Tue 2/18/03 Tue 2/18/03 Tue 2/18/03 Wed 2/26/03 Thu 2/27/03 Thu 4/10/03 Tue 4/15/03 Thu 4/17/03 Wed 4/23/03 Fri 4/25/03 Fri 4/25/03 Wed 4/30/03 Thu 5/01/03 Tue 5/6/03 Thu 5/8/03 Sun 5/19/03 Thu 5/23/03 ¿Questions?