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Protecting flight hardware during spacecraft vibration testing through greater understanding of the CONTRL systems ability to control input and limit responses
Spacecraft level vibration testing exposes the as-built spacecraft, in its flight configuration, to the low frequency (<100 Hz) dynamic environment experienced during launch with the primary objective of verifying structural integrity and system performance. This test requires as flight-like of a configuration as possible and is therefore typically one of the last tests performed in the spacecraft verification program. At this level of integration (spacecraft), failures pose a much greater risk to the program than at lower l ...
Conkey, Shelly; Schaefer, Ed; Persons, David;
Published by: 30th Space Simulation Conference: Mission Success Through Testing of Critical Challenges Published on:
Ability testing; Environmental testing; Software testing; Spacecraft; Vibration analysis; Vibration control; Parker Engineering