The Earth Observing System (EOS) and Space Station (SS) attached payload instruments to be developed by JPL will have a consistent implied level of reliability confidence based on the application of product assurance requirements. An important subset of these requirements is a set of detailed environmental design and test requirements. These requirements have a sound technical defense, are unambiguous in their level of detail, provide rational risk management as a function of payload classification, and are rigorously enforced with a comprehensive waiver process imposed on planned deviations.
Flight payloads environmental approach
Aerospace Testing Seminar ; 1990 ; Manhattan Beach, CA, United States
1990-01-01
Conference paper
No indication
English
The Recovery of Flight Test Payloads
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