Aeroshell structural development for Mars flyby and entry landing mission compatible with Atlas/Centaur launch vehicle
Aeroshell structural development for Martian entry.
AMERICAN INST. OF AERONAUTICS, AND ASTRONAUTICS, ENTRY VEHICLE SYSTEMS AND TECHNOLOGY MEETING ; 1968 ; WILLIAMSBURG, VA
1968-12-01
Conference paper
No indication
English
Aeroshell structural development for Martian entry
AIAA | 1968
|Design of a Mars entry 'Aeroshell'
Tema Archive | 1974
|