Exhibit C
Subsystem
ACS (cont)
Generic Test #
132
132
132
132
115
Test
Pointing/BIAS
Mode Switching
Moon Discrimination
Earth Sensor Preamplifier Output Beacon Mode
Acquisition Pointing/BIAS
Mode Switching
Relative Rate Mode
Relative Rate Toggle
Pseudo Earth Mode
Torque/Pointing Calibrations
Motor Voltage
Torque Calibrations. Pointing Calibration
BAPTA Friction Torque MIP Verification
Stall Torque
Track system integration verification
Battery Controller Power Functional
Bus Overvoltage
Bus Undervoltage
Solar panel functional
Solar Panel Pulsed Xenon Test
Battery Heater Controller
Spacecraft Fuses
122
122
123
137
Power
300
315
320
305
Bus Limiter Operation
335
TBS
330
355
Propulsion
TBS
Valve Electrical
TBS
TBS
TBS
TBS
TBS
TBS
Mechanisms
405
TBS
410
Heater
Visual Examination
Valve Functional
Thruster Valve Leakage
Propulsion Monitoring
Fill and Drain Valve Leak Check
Antenna Positioner Mechanism
Deployment Verification
Omni Deployment
Solar Drum Positioner
Structure
4.
Systems Tests
Deployment Verification
TBS
Grounding Checks, Conductivities
·
The Spacecraft will undergo system level tests following arrival at the launch site. The tests to be performed make up the Launch Site Systems Performance Tests (LSSPT) that
done prior to each HS 376 launch. The tests are as follows.
are
C-4
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