Soft landing spacecraft landing gear design for legged assemblies, discussing load, clearance and stability requirements
Some basic guidelines for establishing structural design parameters for the landing gear of stable, soft landing spacecraft.
STRUCTURES, STRUCTURAL DYNAMICS AND MATERIALS CONFERENCE ; 1968 ; PALM SPRINGS, CA, US
1968-04-01
Conference paper
No indication
English
NTIS | 1979
|NTIS | 1979
|