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A 156-in.-dia SRM mass properties reportMass property data for the 156-in.-dia SRM booster with two segments are presented. The SRM baseline booster has a fixed 15 deg canted nozzle and no thrust neutralization system. Summary mass property data for alternative booster configurations are included.
Document ID
19720021139
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
August 6, 2013
Publication Date
March 10, 1972
Subject Category
Propulsion Systems
Report/Patent Number
REPT-1917-MP1
NASA-CR-123727
Report Number: REPT-1917-MP1
Report Number: NASA-CR-123727
Accession Number
72N28789
Funding Number(s)
CONTRACT_GRANT: NAS8-28428
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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