Dynamics of Lunar Excursion Module following initial landing impact are examined; effects of assumed lunar surface model and important design features of alightment system are described; stability and energy absorption boundaries are established, and comparison is made between predicted boundaries and those obtained from test of 1/6-scale drop test model.
Landing dynamics of lunar excursion module
J Spacecraft Rockets
Journal of Spacecraft and Rockets ; 3 , n 10
1966
6 pages
Aufsatz (Zeitschrift)
Englisch
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Landing dynamics of the Lunar Excursion Module.
NTRS | 1966
|LANDING DYNAMICS OF THE LUNAR EXCURSION MODULE
AIAA | 1966
|Landing dynamics of the lunar excursion module.
NTRS | 1966
|Landing dynamics of the Lunar Excursion Module.
AIAA | 1966
|Lunar excursion module radar receivers.
NTRS | 1966
|