Flight payloads environmental approach
Abstract
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.
- Publication:
-
IN: Aerospace Testing Seminar
- Pub Date:
- 1990
- Bibcode:
- 1990aets.proc..157S
- Keywords:
-
- Earth Observing System (Eos);
- Earth Orbital Environments;
- Space Station Payloads;
- Spacecraft Environments;
- Spacecraft Instruments;
- Design To Cost;
- Earth Observations (From Space);
- Environmental Tests;
- Failure Analysis;
- Orbital Servicing;
- Spacecraft Instrumentation