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  • Other Sources  (3)
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  • 1
    facet.materialart.
    Unknown
    Oxidation protected carbon-carbon (1972)
    In:  CASI
    Details
    Publication Date: 2005-11-30
    Description: Pyrolized carbon-carbon has one unique advantage over other materials that makes its application to the space shuttle thermal protection system very attractive. This unique characteristic is the increase in material strength and modulus with increase in temperature up to about 2500 K (4040 F). Offsetting this unique advantage are disadvantages which include brittleness, high cost, and the tendency of the material to react with oxygen, particularly at high temperatures. The development of an oxidation inhibitor for the material and the definition of fabrication processes for selected full-scale components are considered.
    Keywords: THERMODYNAMICS AND COMBUSTION
    Type: NASA Space Shuttle Technol. Conf.; p 335-372
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
    facet.materialart.
    Unknown
    Structural materials. (1964)
    In:  Other Sources
    Details
    Publication Date: 2018-12-01
    Description: Failure modes of structural materials for manned spacecraft, considering effects of space environment
    Keywords: MATERIALS, METALLIC
    Format: text
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    NASA TECHNICAL REPORTS
  • 3
    facet.materialart.
    Unknown
    Mercury spacecraft structural development problems (1961)
    In:  CASI
    Details
    Publication Date: 2019-08-13
    Keywords: unknown
    Type: NASA-IND. APOLLO TECH. CONF., PT. 2 20 JUL. 1961; P 31-40
    Format: text
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    NASA TECHNICAL REPORTS
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