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Restartable solid motor stage for shuttle applicationsThe application of restartable solid motor stages to shuttle missions has been shown to provide a viable supplement to the shuttle program. Restartable solid motors in the 3000 pound class provide a small expendable transfer stage that reduces the demand on the shuttle for the lower energy missions. Shuttle operational requirements and preliminary performance data provided an input for defining design features required for restartable solid motor applications. These data provided a basis for a configuration definition that is compatible with shuttle operations. Mission by mission analysis showed the impact on a NASA supplied mission model. The results showed a 15% reduction in the number of shuttle flights required. In addition the amount of shuttle capability used to complete the mission objectives was significantly reduced. For example, in the 1979 missions there was a 62% reduction in shuttle capability used. The study also showed that the solid motor could provide a supplement to the TUG that would allow TUGS to be used in a recoverable rather than an expendable mode. The study shows a 71% reduction in the number of TUGs that would be expended.
Document ID
19740028513
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rohrbaugh, D. J.
(Boeing Co. Seattle, Wash., United States)
Date Acquired
August 7, 2013
Publication Date
November 1, 1973
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 73-1240
Meeting Information
Meeting: Propulsion Conference
Location: Las Vegas, NV
Country: US
Start Date: November 5, 1973
End Date: November 7, 1973
Sponsors: American Institute of Aeronautics and Astronautics, Society of Automotive Engineers
Accession Number
74A11263
Funding Number(s)
CONTRACT_GRANT: NAS2-6518
Distribution Limits
Public
Copyright
Other

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