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Volume 38 Issue 4
Apr.  2012
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Journal of Beijing University of Aeronautics and Astronautics  > 2012  >  (4): 487-490,496.
Zhu Hao, Tian Hui, Cai Guobiaoet al. Application of hybrid rocket motor on manned lunar landing[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (4): 487-490,496. (in Chinese)
Citation: Zhu Hao, Tian Hui, Cai Guobiaoet al. Application of hybrid rocket motor on manned lunar landing[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (4): 487-490,496. (in Chinese)
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Application of hybrid rocket motor on manned lunar landing

  • School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 21 Dec 2011
  • Publish Date: 30 Apr 2012
    Abstract
  • A primary optimal design of manned lunar ship with hybrid propulsion system was proposed. After researching on the manned lunar plans of the main space industry countries and regions and analysis of "Apollo" lunar module, based on hybrid rocket motor system design model, a genetic arithmetic was used to optimize the hybrid rocket motors substituting the descent and ascent liquid rocket motors of "Apollo" lunar module. The comparison and analysis of their function, mass, volume and propellant characteristics show that it has great advantages and application prospect for hybrid propulsion technology to be used in manned lunar ship and deep space exploration.

     

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