Effect of shock precursor absorption on superorbital entry heating.
LASHER, L. E., WILSON, K. H. /LOCKHEED AIRCRAFT CORP., RESEARCH LABS., PALO ALTO, CALIF./.
AIAA Journal ; 6 , 12 ; 2419-2420
1968
Article (Journal)
Electronic Resource
English
Non-lifting entry-vehicle design for superorbital velocities
Engineering Index Backfile | 1963
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