PSSC Testbed design

0020-EX-ST-2008 Images

Aerospace Corporation, THE

2008-01-10ELS_87149

PSSC / PSRP Phase 2 12/12/07 david.a.hinkley@aero.org Satellite Design – Exterior View NOTE: • Safety premise: Aluminum satellite body Ejection Direction is a Faraday cage Sun sensor (1 of 4) +Z direction Earth sensor (1 of 4) Rotation axis Rocket nozzle (1 of 4 on this end, Thermal 1 of 8 total) mgmt tape Rocket inhibit plungers 4-cell solar array (1 of 4) -Z direction Thermal mgmt tape Camera (1 of 2) Power-on inhibit 915 MHz patch antenna plungers Engineering and Technology Group ©2007, The Aerospace Corporation, All Rights Reserved 3


Document Created: 2008-01-10 11:35:40
Document Modified: 2008-01-10 11:35:40
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