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
01.01.1973
Sonstige
Keine Angabe
Englisch
Space Shuttle Orbiter payload bay door mechanisms
NTRS | 1979
|Space Shuttle development update
NTRS | 1984
|NTRS | 1979
|Space shuttle nozzle development
Tema Archiv | 1978
|