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Report, status, mass properties for phase A/B study for a pressure fed engine on a reusable space shuttle boosterThe engine weight, mass properties data, and engine design criteria and specifications are presented for a 1.2 million-lb sea-level thrust pressure-fed LOX/RP-1 engine. Engine trade study weight data are included.
Document ID
19720018050
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 2, 2013
Publication Date
March 15, 1972
Subject Category
Propulsion Systems
Report/Patent Number
REPT-9755-72-5
NASA-CR-123638
MSFC-SE-019-014-2H
Report Number: NASA-CR-123638
Report Number: REPT-9755-72-5
Report Number: MSFC-SE-019-014-2H
Accession Number
72N25700
Funding Number(s)
CONTRACT_GRANT: NAS8-28217
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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