Theoretical investigation of entry vehicle stability in the Mars atmosphere.
KYRISS, C. L., RIE, H. /GENERAL ELECTRIC CO., MISSILE AND SPACE DIV.,RE-ENTRY SYSTEMS DEPT., THEORETICAL AERODYNAMI
JOURNAL OF SPACECRAFT AND ROCKETS ; 4 , 2 ; 272-275
1967-01-01
4 pages
Article (Journal)
Electronic Resource
English
Mars Pathfinder Atmosphere Entry Trajectory Design
NTRS | 1995
|Minimum heat input optimal entry into Mars atmosphere
AIAA | 1995
|