Application of hybrid rocket motor on manned lunar landing

Research output: Contribution to journalArticlepeer-review

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.

Original languageEnglish
Pages (from-to)487-490+496
JournalBeijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
Volume38
Issue number4
StatePublished - Apr 2012

Keywords

  • Hybrid rocket motor
  • Manned lunar landing
  • Optimal design

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