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NASA NTRS · 19730003165

Accelerated life testing of spacecraft subsystems

Abstract

The rationale and requirements for conducting accelerated life tests on electronic subsystems of spacecraft are presented. A method for applying data on the reliability and temperature sensitivity of the parts contained in a sybsystem to the selection of accelerated life test parameters is described. Additional considerations affecting the formulation of test requirements are identified, and practical limitations of accelerated aging are described.

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BibTeXRIS

Wiksten, D., Swanson, J.. 1972-11-01. Accelerated life testing of spacecraft subsystems. https://ntrs.nasa.gov/citations/19730003165

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