NASA NTRS ยท 19730016072
Study of solid rocket motor for space shuttle booster, volume 2, book 3, appendix A
Abstract
A systems requirements analysis for the solid propellant rocket engine to be used with the space shuttle was conducted. The systems analysis was developed to define the physical and functional requirements for the systems and subsystems. The operations analysis was performed to identify the requirements of the various launch operations, mission operations, ground operations, and logistic and flight support concepts.
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1972-03-15. Study of solid rocket motor for space shuttle booster, volume 2, book 3, appendix A. https://ntrs.nasa.gov/citations/19730016072
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