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Advanced Solid Rocket Motor Project StatusThe objectives of the project are the following: (1) to improve system safety and reliability; (2) to improve Space Shuttle Payload performance - 12,000 lb; (3) to optimize program cost; and (4) to promote a competitive solid rocket motor industry. The topics are presented in viewgraph form and include the Advanced Solid Rocket Motor (ASRM) project team, ASRM design, design schedules, and technical issues.
Document ID
19920023036
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Keith Coates (Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Publication Information
Publication: Tenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, Part 1
Subject Category
Spacecraft Propulsion and Power
Report/Patent Number
NASA-CP-3163-PT-1
M-693-PT-1
NAS 1.55:3163-PT-1
Meeting Information
Meeting: Tenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, Part 1
Location: Huntsville, AL
Country: US
Start Date: April 28, 1992
End Date: April 30, 1992
Sponsors: Marshall Space Flight Center
Accession Number
92N32280
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19920023034Collected WorksTenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, Part 1
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