NASA NTRS · 19730016073
Study of solid rocket motor for space, shuttle booster, volume 2, book 4 appendices B thru D
Abstract
The mass properties and related data for the solid propellant rocket engine for use with the space shuttle are presented. Data for three solid propellant rocket engines are provided. The three designs considered are: (1) baseline parallel burn, (2) optional parallel burn, and (3) baseline series burn. Layouts of the respective designs to show design and dimensional data are included.
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1972-03-15. Study of solid rocket motor for space, shuttle booster, volume 2, book 4 appendices B thru D. https://ntrs.nasa.gov/citations/19730016073
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