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Apollo spacecraft engine specific impulse, part 2Specific impulse of LM ascent and descent engines and SM engine
Document ID
19700027045
Document Type
Contractor Report (CR)
Authors
Cuffe, J. P. B.
(Boeing Co. Washington, DC, United States)
Date Acquired
August 5, 2013
Publication Date
October 28, 1968
Subject Category
Propulsion Systems
Report/Patent Number
D2-117060-2-PT-2
NASA-CR-112414
Funding Number(s)
CONTRACT_GRANT: NASW-1650
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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