NASA NTRS · 19690004701
A wind profile for generating control requirements for rocket vehicles using liquid-injection control systems
Abstract
Wind profile developed for calculation of deflection impulse for rocket with liquid injection thrust vector control
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Daniele, C. J., Teren, F.. 1968-12-08. A wind profile for generating control requirements for rocket vehicles using liquid-injection control systems. https://ntrs.nasa.gov/citations/19690004701
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