Static and dynamic performance of air cushion landing system is simulated in computer program that treats four primary ACLS subsystems: fan, feeding system, trunk, and cushion. Configuration of systems is sufficiently general to represent variety of practical designs.
Air cushion landing system
NASA Tech Briefs ; 3 , 2
1978-10-01
Miscellaneous
No indication
English
Parachute and cushion landing system.
AIAA | 1966
|NTRS | 1977
|Air cushion landing system stability study
Tema Archive | 1981
|Development of an Air Cushion Landing System
AIAA | 1973
|