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Orbit transfer vehicle engine study. Phase A: Continuation (study results)Studies included: selection of boost pump designs for low NPSH operation and generation of associated programmatic data; evaluation of OTV engine operation at intermediate thrust levels and impact on programmatics; and assessments of OTV engine operation at idle-mode thrusts under conditions experienced during aerobraking maneuvers of the ABOTV. As a result of the studies, it was recommended that the original OTV boost pump designs be used without change for low NPSH operation. Intermediate thrust operation is feasible for both the expander cycle and staged combustion cycles.
Document ID
19810010689
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
February 28, 1981
Subject Category
Space Transportation
Report/Patent Number
NASA-CR-161668
RI/RD81-120
Report Number: NASA-CR-161668
Report Number: RI/RD81-120
Accession Number
81N19216
Funding Number(s)
CONTRACT_GRANT: NAS8-32996
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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