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Lessons Learned form Selecting and Testing Spaceflight PotentiometersA solar array drive (SAD) was designed for operation on the TOPEX/POSEIDON spacecraft that was launched in August of 1992. The experience gained in selecting, specifying, testing to failure, and redesigning its position sensor produced valuable lessons for future component selection and qualification.
Document ID
20060039763
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
hdl:2014/36672
Authors
Iskenderian, T.
Date Acquired
August 23, 2013
Publication Date
May 1, 1994
Distribution Limits
Public
Copyright
Other
Keywords
TOPEX/POSEIDON redesigning SAD component specification

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