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
01.12.1968
Aufsatz (Konferenz)
Keine Angabe
Englisch
Aeroshell structural development for Martian entry
AIAA | 1968
|Design of a Mars entry 'Aeroshell'
Tema Archiv | 1974
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