NASA NTRS · 19650053010
Powered flight trajectory optimization for lunar and interplanetary transfer.
Abstract
Steepest descent method to compute powered flight trajectory optimization for lunar and interplanetary transfer
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Chuck, W., Rosenbaum, R., Willwerth, R. E.. 1965-09-01. Powered flight trajectory optimization for lunar and interplanetary transfer.. https://ntrs.nasa.gov/citations/19650053010
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