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Matching Records: 234
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Heat Shield Employing Cured Thermal Protection Material Blocks Bonded in a Large-Cell Honeycomb Matrix
Document ID: 20120011903
NTRS Full-Text: Click to View  [PDF Size: 129 KB]
Author: Zell, Peter
Abstract: A document describes a new way to integrate thermal protection materials on external surfaces of hide
Publication Year: 2012
Document Type: NASA Tech Brief
Report/Patent Number: ARC-16018-1
Date Acquired: Jul 31, 2012
Sprayable Phase Change Coating Thermal Protection Material
Document ID: 20130011139
NTRS Full-Text: Click to View  [PDF Size: 173 KB]
Author: Richardson, Rod W.; Hayes, Paul W.; Kaul, Raj
Abstract: NASA has expressed a need for reusable, environmentally friendly, phase change coating that is hide
Publication Year: 2005
Document Type: Technical Report
Report/Patent Number: KSC-2005-001
Date Acquired: Mar 18, 2013
Performance of a Light-Weight Ablative Thermal Protection Material for the Stardust Mission Sample Return Capsule
Document ID: 20070014634
NTRS Full-Text: Click to View  [PDF Size: 1.10 MB]
Author: Covington, M. A.
Abstract: New tests and analyses are reported that were carried out to resolve testing uncertainties in the hide
Publication Year: 2005
Document Type: Conference Paper
Date Acquired: Apr 18, 2007
Flight Performance of an Advanced Thermal Protection Material: Toughened Uni-Piece Fibrous Insulation
Document ID: 20020038764
Author: Leiser, Daniel B.; Gordon, Michael P.; Rasky, Daniel J. (Technical Monitor)
Abstract: The flight performance of a new class of low density, high temperature thermal protection materials hide
Publication Year: 1995
Document Type: Preprint
Date Acquired: Apr 12, 2002
Flight Performance of an Advanced Thermal Protection Material: Toughened Uni-Piece Fibrous Insulation
Document ID: 20020032309
Author: Leiser, Daniel B.; Gordon, Michael P.; Rasky, Daniel J. (Technical Monitor)
Abstract: The flight performance of a new class of low density, high temperature, thermal protection materials hide
Publication Year: 1995
Document Type: Preprint
Date Acquired: Mar 29, 2002
Characterization of advanced flexible thermal protection material for space applications
Document ID: 19930028019
Author: Clayton, Joseph P.; Tinker, Michael L.
Abstract: No Abstract Available
Publication Year: 1992
Document Type: Journal Article
Date Acquired: Dec 28, 1995
Characterization and modeling of an advanced flexible thermal protection material for space applications
Document ID: 19910047222
Author: Clayton, Joseph P.; Tinker, Michael L.
Abstract: This paper describes experimental and analytical characterization of a new flexible thermal hide
Publication Year: 1991
Document Type: Conference Paper
Report/Patent Number: AIAA PAPER 91-1047
Date Acquired: Nov 28, 1995
Hypervelocity impact tests on Space Shuttle Orbiter RCC thermal protection material. [Reinforced Carbon-Carbon laminate]
Document ID: 19780058971
Author: Humes, D. H.
Abstract: It is noted that the Shuttle Orbiter will be more subject to meteoroid impact than previous hide
Publication Year: 1978
Document Type: Journal Article
Date Acquired: Dec 01, 1995
A method for determining structural properties of RCC thermal protection material. [Reinforced Carbon-Carbon]
Document ID: 19780052088
Author: Wakefield, R. M.; Fowler, K. R.
Abstract: A method was developed for evaluation and prediction of effects of oxidation of the graphitic hide
Publication Year: 1978
Document Type: Conference Paper
Report/Patent Number: AIAA PAPER 78-869
Date Acquired: Dec 01, 1995
Space Shuttle Orbiter thermal protection material development and testing
Document ID: 19790033660
Author: Larson, H. K.; Goldstein, H. E.
Abstract: The research work described in the present paper was carried out to develop and evaluate thermal hide
Publication Year: 1978
Document Type: Conference Proceedings
Date Acquired: Dec 01, 1995
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