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Solid rocket booster performance evaluation model. Volume 3: Sample caseThe solid rocket booster performance evaluation model (SRB-11) is used to predict internal ballistics in a sample motor. This motor contains a five segmented grain. The first segment has a 14 pointed star configuration with a web which wraps partially around the forward dome. The other segments are circular in cross-section and are tapered along the interior burning surface. Two of the segments are inhibited on the forward face. The nozzle is not assumed to be submerged. The performance prediction is broken into two simulation parts: the delivered end item specific impulse and the propellant properties which are required as inputs for the internal ballistics module are determined; and the internal ballistics for the entire burn duration of the motor are simulated.
Document ID
19770020239
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
September 7, 1974
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-150337
D256-10020-3-VOL-3
Report Number: NASA-CR-150337
Report Number: D256-10020-3-VOL-3
Accession Number
77N27183
Funding Number(s)
CONTRACT_GRANT: NAS8-29643
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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