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Flight payloads environmental approachThe 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.
Document ID
19910045090
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schlue, John W.
(JPL Pasadena, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Instrumentation
Meeting Information
Meeting: Aerospace Testing Seminar
Location: Manhattan Beach, CA
Country: United States
Start Date: March 13, 1990
End Date: March 15, 1990
Sponsors: Institute of Environmental Sciences and Aerospace Corp.
Accession Number
91A29713
Distribution Limits
Public
Copyright
Other

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