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Advanced Metallic Thermal Protection System DevelopmentA new Adaptable, Robust, Metallic, Operable, Reusable (ARMOR) thermal protection system (TPS) concept has been designed, analyzed, and fabricated. In addition to the inherent tailorable robustness of metallic TPS, ARMOR TPS offers improved features based on lessons learned from previous metallic TPS development efforts. A specific location on a single-stage-to-orbit reusable launch vehicle was selected to develop loads and requirements needed to design prototype ARMOR TPS panels. The design loads include ascent and entry heating rate histories, pressures, acoustics, and accelerations. Additional TPS design issues were identified and discussed. An iterative sizing procedure was used to size the ARMOR TPS panels for thermal and structural loads as part of an integrated TPS/cryogenic tank structural wall. The TPS panels were sized to maintain acceptable temperatures on the underlying structure and to operate under the design structural loading. Detailed creep analyses were also performed on critical components of the ARMOR TPS panels. A lightweight, thermally compliant TPS support system (TPSS) was designed to connect the TPS to the cryogenic tank structure. Four 18-inch-square ARMOR TPS panels were fabricated. Details of the fabrication process are presented. Details of the TPSS for connecting the ARMOR TPS panels to the externally stiffened cryogenic tank structure are also described. Test plans for the fabricated hardware are presented.
Document ID
20020020963
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Blosser, M. L.
(NASA Langley Research Center Hampton, VA United States)
Chen, R. R.
(Lockheed Martin Space Operations United States)
Schmidt, I. H.
(Lockheed Martin Space Operations United States)
Dorsey, J. T.
(NASA Langley Research Center Hampton, VA United States)
Poteet, C. C.
(NASA Langley Research Center Hampton, VA United States)
Bird, R. K.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Metals And Metallic Materials
Report/Patent Number
AIAA Paper 2002-0504
Report Number: AIAA Paper 2002-0504
Meeting Information
Meeting: 40th Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 14, 2002
End Date: January 17, 2002
Distribution Limits
Public
Copyright
Public Use Permitted.
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