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  • 1
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    Hybrid Cryogenic Tank Construction and Method of Manufacture Therefor (2011)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: A lightweight, high-pressure cryogenic tank construction includes an inner layer comprising a matrix of fiber and resin suitable for cryogenic use. An outer layer in intimate contact with the inner layer provides support of the inner layer, and is made of resin composite. The tank is made by placing a fiber preform on a mandrel and infusing the preform with the resin. The infused preform is then encapsulated within the outer layer.
    Keywords: Engineering (General)
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
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    Composite Tanks and Pressure Vessel Development (2002)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: Pressure vessels and tanks are vital to NASA missions. Tanks need to be lightweight and perform under the operational environments. Design and material limitations make it difficult to contain the fuels and oxidizers. Recent interest in 90% Hydrogen Peroxide adds to the challenge of containment. The majority of current tank technologies are not easily adaptable to conformal shapes. The cost of tooling-up for large tanks are magnified by sudden design changes. New launch vehicle concepts may require tanks and pressure vessels of a non-standard configuration. Scaled versions of new tanks have been fabricated and testing has begun. Second and third generation launch vehicles decisions will effect the path of research and development.
    Keywords: Engineering (General)
    Type: Society for the Advancement of Materials and Process Engineering 2002 Conference; May 12, 2002 - May 16, 2002; Long Beach, CA; United States
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    Composite Tank Development (2000)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: This paper presents viewgraphs on composite tank development. There is a need for oxidizer tanks and reliable, lightweight fuel. The need for cost-effective and scalable manufacturing is also evident. In order to achieve these goals, tooling methods for tank development must be applied, methods for producing easily adaptable and scalable vessel liners must be developed, insulation layer or protective barriers for containers must be manufactured, and an appropriate fiber/resin system for composite overwrap structures must be identified.
    Keywords: Engineering (General)
    Type: CDDF-96-02 , SAMPE 2000; May 21, 2000 - May 25, 2000; Long Beach, CA; United States
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
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