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Study of solid rocket motor for space shuttle booster. Volume 4: CostThe cost data for solid propellant rocket engines for use with the space shuttle are presented. The data are based on the selected 156 inch parallel and series burn configurations. Summary cost data are provided for the production of the 120 inch and 260 inch configurations. Graphs depicting parametric cost estimating relationships are included.
Document ID
19730016075
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
NASA-CR-124239
TWR-5672-VOL-4
Report Number: NASA-CR-124239
Report Number: TWR-5672-VOL-4
Accession Number
73N24802
Funding Number(s)
CONTRACT_GRANT: NAS8-28430
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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