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Centaur liquid oxygen boost pump vibration testThe Centaur LOX boost pump was subjected to both the simulated Titan Centaur proof flight and confidence demonstration vibration test levels. For each test level, both sinusoidal and random vibration tests were conducted along each of the three orthogonal axes of the pump and turbine assembly. In addition to these tests, low frequency longitudinal vibration tests for both levels were conducted. All tests were successfully completed without damage to the boost pump.
Document ID
19750019316
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Tang, H. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Mechanical Engineering
Report/Patent Number
E-8427
NASA-TM-X-71774
Report Number: E-8427
Report Number: NASA-TM-X-71774
Accession Number
75N27388
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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