Volume 21 Issue 5
Oct.  2006
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ZHANG Chun-liang, WANG-ping. Flow and performance calculation of absorber/thruster of solar thermal propulsion[J]. Journal of Aerospace Power, 2006, 21(5): 943-948.
Citation: ZHANG Chun-liang, WANG-ping. Flow and performance calculation of absorber/thruster of solar thermal propulsion[J]. Journal of Aerospace Power, 2006, 21(5): 943-948.
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Flow and performance calculation of absorber/thruster of solar thermal propulsion

  • 1.

    School of Space Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • 2.

    The First Aeronautics Institute of PLA Air Force, Xinyang 464000, China

  • Received Date: 2005-09-06
  • Rev Recd Date: 2006-03-06
  • Publish Date: 2006-10-28
    Abstract
  • Based on experimental data about large STP(Solar Thermal Propulsion),structural analysis and experimental condition estimation were made.By means of equal wall-temperature model and FLUENT software,inner-flow,heat-transfer and performance characteristics were calculated.Calculation results are in good agreement with experimental data.It has important meaning for design STP.

     

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    • References(6)
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    王平,张纯良.太阳能火箭发动机推力器内流场模拟研究[D].北京:北京航空航天大学,2004.
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    Shimizu Morio,Itoh Katsuya,Hitoshi Sato,Hitoshi Naito.Large Solar Thermal Thruster Made of Single Crystal Molybdenum[R].51sT International Astronautical Congress,2000/Rio de Janeiro,Brazil.IAF-00-S.6.01.
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    Shimizu M,Itoh K and Sato H.Fabrication and Tests of Single Crystal Mo Solar Thermal Thruster[R].48th International Astronautical Congress,1997/Turin,Italy.IAF97-5.6.03.
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