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Explore the detailed specifications and timeline for the OMEGA Project's mission control system design, including power supply, data processing, electrical, launch, mechanical, thermal, and ozone sensor systems. Follow along as the team progresses towards the launch with careful planning and execution.
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OMEGA PROJECT TEAM: ALPHA Members: Alexandra Salgado Shaun Besse Lizzabeth Ponce
Expected Results Julich Ozone Sonde Intercomparison Experiment
System Design • 1. Power supply system • 2. Data-processing system • 3. Electrical system • 4. Launch system • 5. Mechanical system • 6. Thermal system • 7. Ozone sensor system
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 • . • The mission software • Talks to the sensors.
Launch system Top View ofSpacecraftinterface * 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
Weight Budget 700 g from ACES program office 200 g from Team “JHK” 100 g from Team “Late Ballooners”
Main Schedule Activity Start Finish Mission Objectives Mon 2/3/03 Wed 2/5/03 Project Management Thu 2/6/03 Tue 2/11/03 Payload Design Wed 2/5/03 Thu 2/13/03 Science Abstract and WBS Fri 2/14/03 Fri 2/14/03 Payload Development Plan Thu 2/13/03 Tue 2/18/03 Payload Construction Plan Thu 2/13/03 Tue 2/18/03 Master Budget Thu 2/13/03 Tue 2/18/03 Written PDR Wed 2/19/03 Wed 2/26/03 Preliminary Design Review Thu 2/27/03 Thu 2/27/03 Critical Design Review Thu 4/10/03 Thu 4/10/03 Ordering of Parts Fri 4/11/03 Tue 4/15/03 Fabrication of Payload Box Mon 4/14/03 Thu 4/17/03 Receiving ordered parts Mon 4/20/03 Wed 4/23/03 Build Ozone Sensor system Wed 4/23/03 Fri 4/25/03 Build Electrical system Wed 4/23/03 Fri 4/25/03 Test built systems Sat 4/26/03 Wed 4/30/03 Assemble payload Thu 5/1/03 Thu 5/01/03 Test assembled payload Fri 5/2/03 Tue 5/6/03 Flight Readiness Review (FRR) Thu 5/8/03 Thu 5/8/03 Launch Trip Sun 5/19/03 Thu 5/23/03