Item Details

Coolant-Side Heat-Transfer Rates for a Hydrogen-Oxygen Rocket and a New Technique for Data Correlation

by Ralph L. Schacht and Richard J. Quentmeyer
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973.
Language
English
Series
NASA Technical Note
Description
46 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at Lewis Research Center.
  • Cover title.
  • Bibliography: p. 21-22.
Series Statement
NASA technical note ; NASA TN D-7207
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

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    a| Coolant-side heat-transfer rates for a hydrogen-oxygen rocket and a new technique for data correlation / c| by Ralph L. Schacht and Richard J. Quentmeyer.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration ; a| [Springfield, Va. : b| For sale by the National Technical Information Service], c| 1973.
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    a| 46 p. : b| ill. ; c| 27 cm.
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    a| NASA technical note ; v| NASA TN D-7207
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    a| Prepared at Lewis Research Center.
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    a| Bibliography: p. 21-22.
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    a| Mode of access: Internet.
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    a| Nuclear rockets.
    650
      
    0
    a| Heat x| Transmission.
    650
      
    0
    a| Liquid propellant rockets x| Fuel systems.
    650
      
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    a| Rocket engines x| Thrust.
    650
      
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    a| Rocket engines x| Cooling.
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