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Solid rocket motor certification to meet space shuttle requirements from challenge to achievementThree solid rocket motor (SRM) design requirements for the Space Shuttle were discussed. No existing solid rocket motor experience was available for the requirement for a thrust-time trace, twenty uses for the principle hardware, and a moveable nozzle with an 8 deg. omnivaxial vectoring capability. The solutions to these problems are presented.
Document ID
19850008632
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Miller, J. Q. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Kilminster, J. C. (Thiokol, Inc., Brigham City Utah, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: NASA. Johnson Space Center Space Shuttle Tech. Conf., Pt. 2
Subject Category
Spacecraft Propulsion And Power
Accession Number
85N16941
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19850008628Collected WorksSpace Shuttle Technical Conference, Part 2
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