NASA NTRS · 19680036593
A parametric analysis of three vehicle shapes for use as hyperbolic entry.
Abstract
Apollo command module, biconic and cone hyperbolic reentry vehicles engineering, discussing L/D ratio, heat protection and weight
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Anderson, J. L., Swenson, B. L.. 1968-01-01. A parametric analysis of three vehicle shapes for use as hyperbolic entry.. https://ntrs.nasa.gov/citations/19680036593
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