NASA NTRS · 19690054165
Rocket trajectory optimization by a second- order numerical technique.
Abstract
Multistage rocket trajectories optimized by second order numerical technique and digital computer program, considering coasting, vacuum flight and transition times
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Kelley, H. J., Mckay, S. S., II, Uzzell, B. R.. 1969-05-01. Rocket trajectory optimization by a second- order numerical technique.. https://ntrs.nasa.gov/citations/19690054165
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