NASA NTRS · 19660001347
Study of selected thrust vector control systems for solid propellant motors final report, 2 Jun. - 2 Aug. 1965
Abstract
Thrust vector control for solid propellant rocket engines - liquid injection system, hot or cold gas systems, and gimballed nozzle systems
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1965-08-01. Study of selected thrust vector control systems for solid propellant motors final report, 2 Jun. - 2 Aug. 1965. https://ntrs.nasa.gov/citations/19660001347
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