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The qualification of the shuttle booster separation motorsFour booster separation motors (BSM) located at each end of every solid rocket booster (SRB) provide the needed side force to separate the boosters from the external tank at booster burnout. Four BSMs at the top of the SRB are located in a box pattern in the nose cone frustum. The four BSMs at the aft end of the SRB are arranged side-by-side on the SRB aft skirt. Aspects of BSM design and performance are considered, taking into account a motor design/performance summary, the case design, the insulation, the grain design, the nozzle/aft closure design, the ignition system, the propellant, and the motor assembly. Details of motor testing are also discussed, giving attention to development testing, qualification testing, and flight testing.
Document ID
19780064559
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chase, C. A.
(United Technologies Corp. Sunnyvale, CA, United States)
Fisher, K. M.
(United Technologies Corp. Chemical Systems Div., Sunnyvale, Calif., United States)
Eoff, W.
(NASA Marshall Space Flight Center Huntsville, Ala., United States)
Date Acquired
August 9, 2013
Publication Date
July 1, 1978
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 78-983
Meeting Information
Meeting: Joint Propulsion Conference
Location: Las Vegas, NV
Country: US
Start Date: July 25, 1978
End Date: July 27, 1978
Sponsors: Society of Automotive Engineers, American Institute of Aeronautics and Astronautics
Accession Number
78A48468
Distribution Limits
Public
Copyright
Other

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