Future directions in materials and structures for space applicationsA comprehensive evaluation is made of materials and structural technology requirements for future space transportation systems, large spacecraft, and space structures. Exceptional promise is noted in carbon-carbon composites for large area thermal protection systems. High temperature test facilities, techniques, and instrumentation systems have unfortunately been neglected, and a materials systems data base suitable for high confidence design of long life space structures has yet to be compiled with a view to material environments in low earth and geosynchronous orbits. A coordinated analysis, ground test, and in-orbit experimentation program for candidate structure designs is called for.
Document ID
19860055873
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Venneri, S. L. (NASA Headquarters Washington, DC United States)
Hayduk, R. J. (NASA Headquarters Washington, DC United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 86-1185Report Number: AIAA PAPER 86-1185