NASA NTRS · 19700003019
Thrust vector control requirements for launch vehicles using a 260-inch solid rocket first stage
Abstract
Gimbaled nozzle and liquid injection thrust vector control requirements for solid rocket two stage launch vehicles
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Borsody, J., Daniele, C. J., Scalzott, L. L.. 1969-12-01. Thrust vector control requirements for launch vehicles using a 260-inch solid rocket first stage. https://ntrs.nasa.gov/citations/19700003019
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