NASA NTRS · 19720020171
Study of solid rocket motors for a space shuttle booster, volume 2
Abstract
Additional technical data have been prepared to supplement the data supplied in the SRM shuttle booster final report. These data cover performance characteristics utilizing motor efficiencies of 0.960 and 0.947 with nozzle divergence half angles of 15 deg and 20 deg, respectively; PBAN propellant characteristics; parametric data to extend baseline designs to varying states of SRM's; summary of SRM mass properties; and SRM exhaust plume profiles.
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1972-04-19. Study of solid rocket motors for a space shuttle booster, volume 2. https://ntrs.nasa.gov/citations/19720020171
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