REG NASA-LLIS-1532--2005 Lessons Learned - Space vs Ground Ambient Which Environment is More Severe (2002).pdf
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1、Lessons Learned Entry: 1532Lesson Info:a71 Lesson Number: 1532a71 Lesson Date: 2005-04-25a71 Submitting Organization: JPLa71 Submitted by: David OberhettingerSubject: Space vs. Ground Ambient, Which Environment is More Severe? (2002) Abstract: A test error was suspected during ground performance tes
2、ting of the Tropospheric Emission Spectrometer (TES) until it was determined that the Environmental Requirements Document-specified test limit applied to a different mission phase. Environmental requirements analysis should clearly identify and discriminate between the various specified flight proje
3、ct environments.Description of Driving Event: The Tropospheric Emission Spectrometer (TES) is an Earth observing instrument with focal plane arrays that are mechanically cooled to 63 degrees K. to reduce the instrument thermal background. During ambient performance testing of the instrument (Referen
4、ce (1), several major assemblies violated the upper-limit Allowable Flight Temperature (AFT) and Protoflight (PF) operational temperatures specified by the Environmental Requirements Document (ERD). The ERD (Reference (2) is the JPL document that specifies the environments the mission will encounter
5、; it serves as the basis for the environmental design and test of JPL subsystems and systems, including the specification of test levels and durations. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-refer to D descriptionDIt was determined that the
6、ground test had been performed at an appropriate temperature. The hot operating temperature limit imposed by the ERD was found to pertain solely to the extreme low temperature science data collection periods. The ERD did not specify environmental limits for ambient, “non-science” operating condition
7、s such as the ground environment that was the subject of the test. An ERD typically specifies allowable ground conditions as well as characterizing the spaceflight environment. References:1. JPL Problem/Failure Report No. Z77843, October 8, 2002.2. 3. JPL Environmental Assurance Standard (D-14040),
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