Apollo command module, biconic and cone hyperbolic reentry vehicles engineering, discussing L/D ratio, heat protection and weight
A parametric analysis of three vehicle shapes for use as hyperbolic entry.
AEROSPACE SCIENCES MEETING ; 1968 ; NEW YORK, NY
1968-01-01
Conference paper
No indication
English
Hyperbolic "Smoothing" of Shapes
British Library Conference Proceedings | 1998
|Optimization of entry-vehicle shapes during conceptual design
Online Contents | 2014
|Earth entry at hyperbolic velocities
AIAA | 1968
|Parametric weight study of manned space entry vehicle
Engineering Index Backfile | 1960
|