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  • 1
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    Assessing the orbiter thermal environment using flight data (1984)
    In:  Other Sources
    Details
    Publication Date: 2011-08-19
    Keywords: SPACE TRANSPORTATION
    Type: Journal of Spacecraft and Rockets (ISSN 0022-4650); 21; 534-541
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
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    Columbia: The first 5 flights entry heating data series. Volume 5: The side fuselage and payload bay door (1984)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Entry heating flight data and wind tunnel data on the side fuselage and payload bay door, Z = 400 and 440 trace aft of X/L=0.2, for the first five flights of the Space Shuttle Orbiter are presented. The heating rate data are reviewed in terms of normalized film heat transfer coefficients as a function of angle of attack, Mach number, and normal shock Reynolds number. The surface heatings rates and temperatures were obtained by the JSC NONLIN/INVERSE computer program. Time history plots of the surface heating rates and temperatures are outlined.
    Keywords: SPACE TRANSPORTATION
    Type: NASA-CR-171732 , NAS 1.26:171732 , LEMSCO-19346-VOL-5
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    An assessment of the Space Shuttle Orbiter thermal environment using flight data (1983)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: A unified analysis of the Shuttle Orbiter aerothermodynamic environment and thermal protection system performance is presented using the Space Transportation System development flight data. Comparisons of predicted and measured temperatures and heating rates along the Orbiter lower windward fuselage centerline and lower wing 50 percent and 80 percent semi-spans are discussed. The results of this study indicate lower than predicted heating on windward fuselage surface but higher heating on the nose cap and 50 percent semi-span wing panels.
    Keywords: SPACE TRANSPORTATION
    Type: AIAA PAPER 83-1488
    Format: text
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    NASA TECHNICAL REPORTS
  • 4
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    Columbia: The first five flights. Entry heating data series. Volume 6: The upper leeside surface centerline (1984)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The aerothermodynamic performance of the Space Shuttle Orbiter during reentry is assessed from the collected data of the first five flights. The entry heating data is restricted to the upper leeside surface centerline of the orbiter. Surface heating and temperature data are analyzed by a variety of computer programs and presented in graphic form. Wind tunnel test data is also included.
    Keywords: SPACE TRANSPORTATION
    Type: NASA-CR-171795 , NAS 1.26:171795 , LEMSCO-19346-VOL-6
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 5
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    User's guide for CCT2WA (converting CCT's to work-addressable file) (1981)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The CCT2WA program, developed to convert the shuttle post-flight computer compatible tape data to a word addressable mass storage file, is described. The use of utility processors that can be used to copy word addressable files from mass storage to mass storage is also described.
    Keywords: COMPUTER PROGRAMMING AND SOFTWARE
    Type: NASA-CR-161076 , JSC-17377
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 6
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    Columbia: The first 5 flights entry heating data series. Volume 1: An overview (1984)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Entry heating flight data and wind tunnel data on the lower windward and upper lee side centerline, lower wing 50% and 80% semi-spans, side fuselage and payload bay door, Z-400 and 440 trace aft of X/L=0.2, and OMS Pod trace 3, are presented for the first five flights of the space shuttle orbiter. Heating rate distributions are presented in terms of normalized shock Reynolds number to show the sensitivity of heating to these parameters. The surface heating rates and temperatures were obtained via the JSC NONLIN/INVERSE computer program.
    Keywords: SPACE TRANSPORTATION
    Type: NASA-CR-171820 , NAS 1.26:171820 , LEMSCO-19346-VOL-1
    Format: application/pdf
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  • 7
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    Columbia: The first five flights entry heating data series. Volume 2: The OMS Pod (1983)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Entry heating flight data and wind tunnel data on the OMS Pod are presented for the first five flights of the Space Shuttle Orbiter. The heating rate data are presented in terms of normalized film heat transfer coefficients as a function of angle-of-attack, Mach number, and normal shock Reynolds number. The surface heating rates and temperatures were obtained via the JSC NONLIN/INVERSE computer program. Time history plots of the surface heating rates and temperatures are also presented.
    Keywords: SPACE TRANSPORTATION
    Type: NASA-CR-171657 , NAS 1.26:171657 , LEMSCO-19346-VOL-2
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 8
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    Columbia: The first five flights entry heating data series. Volume 3: The lower windward surface centerline (1983)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Entry heating flight data and wind tunnel data on the lower surface centerline are presented in terms of normalized film heat transfer coefficients as a function of angle-of-attack, Mach number, and Normal Shock Reynolds number. The surface heating rates and temperatures were obtained via the JSC NONLIN/INVERSE computer program. Time history plots of the surface heating rates and temperatures are also presented.
    Keywords: SPACE TRANSPORTATION
    Type: NASA-CR-171665 , NAS 1.26:171665 , LEMSCO-19346-VOL-3
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 9
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    Columbia: The first five flights entry heating data series. Volume 4: The lower windward wing 50 percent and 80 percent semispans (1983)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: Entry heating flight data and wind tunnel data on the lower wing 50% and 80% Semi-Spans are presented for the first five flights of the Space Shuttle Orbiter. The heating rate data is presented in terms of normalized film heat transfer coefficients as a function of angle-of-attack, Mach number, and Normal Shock Reynolds number. The surface heating rates and temperatures were obtained via the JSC NONLIN/INVERSE computer program. Time history plots of the surface heating rates and temperatures are also presented.
    Keywords: SPACE TRANSPORTATION
    Type: NASA-CR-171666 , NAS 1.26:171666 , LEMSCO-19346-VOL-4
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 10
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    An implicit formulation for the one-dimensional two-phase multi-interface Stefan Problem (1982)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: In recent years there has been an intensified effort in the analysis of the Stefan Problem. Particular interest is directed towards determining the location of the interface between the solid and liquid phases of the substance being analyzed. A method has been developed using an implicit finite difference scheme which provides an accurate calculation of the phase change interface locations for a problem with simultaneous multiple phases. This is achieved through an iterative technique which requires the phase change energy to be correctly distributed within the nodes which are undergoing a phase transition. The new method predicts the interface locations without requiring time step size control or node size modification at the interfaces.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: ASME PAPER 82-HT-21 , American Institute of Aeronautics and Astronautics and American Society of Mechanical Engineers, Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference; Jun 07, 1982 - Jun 11, 1982; St. Louis, MO
    Format: text
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