Design and testing of a hot redundant structure concept for a hypersonic flight vehicle.
BARRETT, W. F., MCCOWN, J. W., NORTON, A. M. /MARTIN MARIETTA CORP., MARTIN CO., SPACE SYSTEMS DIV., VEHICLE DESIGN DEPT., BALTIMOR
JOURNAL OF SPACECRAFT AND ROCKETS ; 3 , 5 ; 685-692
1966-01-01
8 pages
Article (Journal)
Electronic Resource
English
Design and testing of hot redundant structure concept for hypersonic flight vehicle
Engineering Index Backfile | 1966
|NTIS | 1987
|NTIS | 1994
|AIAA | 1992
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