NASA NTRS · 19850008632
Solid rocket motor certification to meet space shuttle requirements from challenge to achievement
Abstract
Three 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.
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Miller, J. Q., Kilminster, J. C.. 1985-01-01. Solid rocket motor certification to meet space shuttle requirements from challenge to achievement. https://ntrs.nasa.gov/citations/19850008632
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