Entry corridor thermal entry limits for Apollo spacecraft defined for design of thermal protection system
Definition of entry corridor thermal limits for Apollo spacecraft.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ENTRY VEHICLE SYSTEMS AND TECHNOLOGY MEETING ; 1968 ; WILLIAMSBURG, VA
1968-12-01
Conference paper
No indication
English
Engineering Index Backfile | 1964
|NTRS | 1969
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