REG NASA-LLIS-0272--1993 Lessons Learned Flight Anomaly of Atmospheric Trace Molecule Spectroscopy (ATMOS) Instrument Risk Assessment.pdf
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1、Lessons Learned Entry: 0272Lesson Info:a71 Lesson Number: 0272a71 Lesson Date: 1993-07-08a71 Submitting Organization: JPLa71 Submitted by: P. W. SchaperSubject: Flight Anomaly of Atmospheric Trace Molecule Spectroscopy (ATMOS) Instrument, Risk Assessment Abstract: The ATMOS instrument experienced a
2、randomly occurring failure on the ground that was fixed each time by resetting the instrument. After an extended investigation that failed to identify the failure mechanism, the workaround was employed successfully on repeated Shuttle flights.For low-cost, reflyable experiments, generate preplanned
3、in-flight workaround procedures for random performance anomalies to enable successful repeated flights, consider cost tradeoffs in risk assessments, and view the testing and qualification rules established for single flight projects as guidelines only.Description of Driving Event: On March 24, 1992
4、the ATMOS instrument, a fourier transform spectrometer, flew on the Atmospheric Laboratory for Applications and Science (ATLAS 1) payload aboard the shuttle (STS) Atlantis with an open problem/failure report (PFR). The events leading to this state of readiness can be briefly summarized as follows: s
5、ince the experiment for which this instrument was built was proposed as a low cost effort at a very early time in the STS program, the proposal did not plan for a breadboard or prototype model. The instrument had its maiden flight on the SPACELAB 3 mission in 1985 and was expected to be reflown seve
6、ral more times at 12 month intervals on STS missions. During the hiatus of reflights, caused by the Challenger accident, ATMOS was extensively used for making significant ground based observations. During these operations an infrequent, and apparently randomly occurring failure was observed in the s
7、tartup sequence, in that the moving slides stopped. The failure could always be overcome by resetting the instrument. In spite of concerted efforts to isolate the cause of this anomaly, the failure mechanism was not identified even though certain suspect parts were exchanged. An in-flight workaround
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