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Study of solid rocket motors for a space shuttle booster, volume 2Additional technical data have been prepared to supplement the data supplied in the SRM shuttle booster final report. These data cover performance characteristics utilizing motor efficiencies of 0.960 and 0.947 with nozzle divergence half angles of 15 deg and 20 deg, respectively; PBAN propellant characteristics; parametric data to extend baseline designs to varying states of SRM's; summary of SRM mass properties; and SRM exhaust plume profiles.
Document ID
19720020171
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
August 6, 2013
Publication Date
April 19, 1972
Subject Category
Propulsion Systems
Report/Patent Number
UTC-4205-72-7-VOL-2-ADD-1
NASA-CR-127416
Report Number: UTC-4205-72-7-VOL-2-ADD-1
Report Number: NASA-CR-127416
Accession Number
72N27821
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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