Monte Carlo dynamic analysis for lunar module landing loads
MERCHANT, D. H., SAWDY, D. T. /BOEING CO., AEROSPACE GROUP, HOUSTON, TEX./.
JOURNAL OF SPACECRAFT AND ROCKETS ; 8 , 1 ; 48-55
1971-01-01
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
The Use of Monte Carlo Simulation in Determining Landing Gear Loads during Landing
British Library Conference Proceedings | 1991
|Apollo Lunar Module Landing Gear
NTRS | 1972
|