The results of development of an advanced composite door landing-gear assembly are summarized. The development program consisted of design, analysis, fabrication, and structural testing of a door sector assembly designed to the operating loads expected for the Phase B Space Shuttle orbiter.
Graphite-epoxy door development for application to Space Shuttle.
National Symposium and Exhibition on New horizons in materials and processing ; 1973 ; Los Angeles, CA
1973-01-01
Miscellaneous
No indication
English
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