Structural design options for decelerative aeroshell configurations for atmospheric entry on unmanned planetary explorations
Structural and decelerator design options for Mars entry.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AND AMERICAN SOCIETY OF MECHANICAL ENGINEERS, STRUCTURES, STRUCTURAL DYNAMICS AND MATERIALS CONFERENCE ; 1968 ; PALM SPRINGS, CALIF.
1969-01-01
Miscellaneous
No indication
English
Structural and decelerator design options for Mars entry
Engineering Index Backfile | 1969
|Uncertainty Analysis of Mars Entry Flows over a Hypersonic Inflatable Aerodynamic Decelerator
Online Contents | 2015
|