NASA NTRS · 19740023190
Research on development of equations for performance trajectory computation
Abstract
A computer program for computing the performance trajectory of spacecraft was developed. An analytical study of a minimum fuel flight for high speed aircraft was conducted. The computer program to compute a minimum time reentry into the atmosphere for an Apollo-type capsule is presented. A technical summary of the minimum fuel problem is provided.
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Harmon, G. R.. 1974-01-01. Research on development of equations for performance trajectory computation. https://ntrs.nasa.gov/citations/19740023190
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