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  • 1
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    Hyper-X Hot Structures Comparison of Thermal Analysis and Flight Data (2004)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: The Hyper-X (X-43A) program is a flight experiment to demonstrate scramjet performance and operability under controlled powered free-flight conditions at Mach 7 and 10. The Mach 7 flight was successfully completed on March 27, 2004. Thermocouple instrumentation in the hot structures (nose, horizontal tail, and vertical tail) recorded the flight thermal response of these components. Preflight thermal analysis was performed for design and risk assessment purposes. This paper will present a comparison of the preflight thermal analysis and the recorded flight data.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: Paper 109-A0016 , Fifteenth Annual Thermal and Fluids Analysis Workshop; Aug 29, 2004 - Sep 03, 2004; Pasadena, CA; United States
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
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    NASA Glenn Steady-State Heat Pipe Code Users Manual, DOS Input (2000)
    In:  CASI
    Details
    Publication Date: 2019-07-10
    Description: The heat pipe code LERCHP has been revised, corrected, and extended. New features include provisions for pipes with curvature and bends in "G" fields. Heat pipe limits are examined in detail and limit envelopes are shown for some sodium and lithium-filled heat pipes. Refluxing heat pipes and gas-loaded or variable conductance heat pipes were not considered.
    Keywords: Fluid Mechanics and Thermodynamics
    Type: NASA/TM-2000-209807 , E-12113 , NAS 1.15:209807
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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