LAC Test Descriptions
Vibration:
- Individual Modules Tested to Proto-flight Level (1.25 X Expected Maximum Flight Loads)
- Instrument Mounted on Spacecraft and Tested to Flight Level
Thermal Vacuum (Pre-spacecraft Integration):
- Four Cycles to Survival Levels (-10° C to + 50° C; Range Expected on Orbit 20° C ± 10° C )
- Operation from 0° C to 30° C (Orbital Predict 20° C, 30° C Worst Case)
- Images Obtained Using LAC GSE
Thermal Vacuum (Integrated with Spacecraft):
- Four Cycles
- Operation from 0° C to 30° C (No Operation at 40° C)
- Images Using Spacecraft System (WARP, XPAA, etc.)