NASA NTRS · 19730048256
Graphite-epoxy door development for application to Space Shuttle.
Abstract
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.
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Kam, C. Y., Kong, S. J., Freeman, V. L.. 1973-01-01. Graphite-epoxy door development for application to Space Shuttle.. https://ntrs.nasa.gov/citations/19730048256
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