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Integrated Advanced Microwave Sounding Unit-A (AMSU-A). Engineering Test Report: AMSU-A1 EOS Instrument, (S/N 202) Qualification Level Vibration Tests of August/September 1998, (S/O 565632, OC-417) Plus Addendum AThe purpose of this report is to present a qualification level vibration testing performed on the S/N 202, EOS AMSU-A1 Instrument was vibration tested to qualification levels per the Ref. 1 shop order. The instrument withstood the 8 g sine sweep test, the 7.5 Grms random vibration test, and the 18.75 g sine burst test in each of the three orthogonal axes. Some loss of transmissibility, however, is seen in the lower reflector after Z-axis random vibration. The test sequence was not without incidence. Failure of Channel 7 in the Limited Performance Test (LPT) performed after completion of the 1 st (X-axis) axis vibration sequence, required replacement of the DRO and subsequent re-testing of the instrument. The post-vibration comprehensive performance test (CPT) was successfully run after completion of the three axes of vibration with the replacement component installed in the instrument. Passing the CPT signified the successful completion of the S/N 202 A1 qualification vibration testing.
Document ID
19990068741
Acquisition Source
Goddard Space Flight Center
Document Type
Contractor Report (CR)
Authors
Heffer, R.
(GenCorp Aerojet Azusa, CA United States)
Date Acquired
September 6, 2013
Publication Date
November 10, 1998
Subject Category
Computer Programming And Software
Report/Patent Number
AEROJET-11318
NAS 1.26:209214
NASA/CR-1998-209214
CDRL-207
Funding Number(s)
CONTRACT_GRANT: NAS5-32314
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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