Graphite-epoxy door development for application to Space Shuttle.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.
Document ID
19730048256
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Kam, C. Y.
Kong, S. J.
Freeman, V. L. (McDonnell Douglas Astronautics Co. Huntington Beach, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Subject Category
Materials, Nonmetallic
Meeting Information
Meeting: National Symposium and Exhibition on New horizons in materials and processing