NASA NTRS · 19680026605
A semigraphical method for a deorbit trajectory design study
Abstract
Semigraphical method to aid selection of descent trajectory compatible with mission constraints
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Green, R. N., Hampshire, W. F., II, Souders, S. W.. 1968-10-01. A semigraphical method for a deorbit trajectory design study. https://ntrs.nasa.gov/citations/19680026605
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