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Multiwall TPS - An emerging conceptResearch on titanium multiwall used for thermal protection is reviewed. Continuing analytical and experimental studies yielding a fundamental understanding of the thermal and structural performance of the basic multiwall concept are presented noting that central to this understanding is a knowledge of the extensional behavior of the dimpled sheets since the thinner flat sheets will buckle and be relatively ineffective in supporting compressive loads. Results from radiant heating, aerothermal, vibration, acoustic and lightning strike tests are described as part of an effort to verify the performance of multiwall tiles under representative operating conditions. Flight tests of a large array of tiles are also planned as part of an orbiter experiments program. The research effort is being extended from flat all-titanium multiwall configurations limited to temperatures below 810 K to curved surfaces and higher temperature versions. Multi-wall concepts are found to offer the durability of metallic systems and to be mass competitive with the insulation system currently used on the Space Shuttle Orbiter.
Document ID
19810045011
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Shideler, J. L.
(NASA Langley Research Center Hampton, VA, United States)
Kelly, H. N.
(NASA Langley Research Center Hampton, VA, United States)
Avery, D. E.
(NASA Langley Research Center Hampton, VA, United States)
Blosser, M. L.
(NASA Langley Research Center Hampton, VA, United States)
Adelman, H. M.
(NASA Langley Research Center Loads and Aeroelasticity Div., Hampton, Va., United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1981
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 81-0586
Meeting Information
Meeting: Conference on Structures, Structural Dynamics and Materials
Location: Atlanta, GA
Start Date: April 6, 1981
End Date: April 8, 1981
Accession Number
81A29415
Distribution Limits
Public
Copyright
Other

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