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
01.12.1968
Aufsatz (Konferenz)
Keine Angabe
Englisch
Engineering Index Backfile | 1964
|NTRS | 1969
|