PSSC design

0024-EX-PL-2008 Images

Aerospace Corporation, THE

2008-01-10

  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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