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SSME Alternate Turbopump Development Program: Design verification specification for high-pressure fuel turbopumpThe design and verification requirements are defined which are appropriate to hardware at the detail, subassembly, component, and engine levels and to correlate these requirements to the development demonstrations which provides verification that design objectives are achieved. The high pressure fuel turbopump requirements verification matrix provides correlation between design requirements and the tests required to verify that the requirement have been met.
Document ID
19900000717
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 6, 2013
Publication Date
April 21, 1989
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
DVS-30-REV-3
NAS 1.26:183676
NASA-CR-183676
Report Number: DVS-30-REV-3
Report Number: NAS 1.26:183676
Report Number: NASA-CR-183676
Accession Number
90N10033
Funding Number(s)
CONTRACT_GRANT: NAS8-36801
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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