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  • 1970-1974  (3)
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  • 1
    facet.materialart.
    Unknown
    Scramjet nozzle design and analysis as applied to a highly integrated hypersonic research airplane (1974)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: The configuration and performance of the propulsion system for the hypersonic research vehicle are discussed. A study of the interactions between propulsion and aerodynamics of the highly integrated vehicle was conducted. The hypersonic research vehicle is configured to test the technology of structural and thermal protection systems concepts and the operation of the propulsion system under true flight conditions for most of the hypersonic flight regime. The subjects considered are: (1) research vehicle and scramjet engine configurations to determine fundamental engine sizing constraints, (2) analytical methods for computing airframe and propulsion system components, and (3) characteristics of a candidate nozzle to investigate vehicle stability and acceleration performance.
    Keywords: AIRCRAFT PROPULSION AND POWER
    Type: NASA-TM-X-71972
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
    facet.materialart.
    Unknown
    Aerodynamic characteristics of a hypersonic transport configuration at Mach 6.86 (1970)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: Aerodynamic characteristics of hypersonic transport configuration at Mach 6.86
    Keywords: AERODYNAMICS
    Type: NASA-TN-D-5885 , L-6803
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    Unknown
    Potential of hydrogen fuel for future air transportation systems. (1973)
    In:  Other Sources
    Details
    Publication Date: 2019-07-27
    Description: Recent studies have shown that hydrogen fuel can yield spectacular improvements in aircraft performance in addition to its more widely discussed environmental advantages. The characteristics of subsonic, supersonic, and hypersonic transport aircraft using hydrogen fuel are discussed, and their performance and environmental impact are compared to that of similar aircraft using conventional fuel. The possibilities of developing hydrogen-fueled supersonic and hypersonic vehicles with sonic boom levels acceptable for overland flight are also explored.
    Keywords: PROPELLANTS
    Type: ASME PAPER 73-ICT-104 , Intersociety Conference on Transportation; Sept. 23-27, 1973; Denver, CO
    Format: text
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    NASA TECHNICAL REPORTS
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