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Experimental study on the working performance of powdered magnesium and liquid carbon dioxide bipropellant rocket engine for Mars missions

  • Published:2021-07 Issue: Volume:184 Page:274-285
  • ISSN:0094-5765
  • Container-title:Acta Astronautica
  • language:en
  • Short-container-title:Acta Astronautica

Author:

Hu JiamingORCID,Hu Chunbo,Che YanhongORCID,Zhu Xiaofei,Yang Jiangang,Li Mengzhe,Li Chao

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference40 articles.

1. Integrated in-situ resource utilization system design and logistics for Mars exploration[J];Chen;Acta Astronaut.,2020

2. An ISRU Propellant Production System to Fully Fuel a Mars Ascent vehicle[R];Kleinhenz,2017

3. Technology development for human exploration of Mars[J];Moore;Acta Astronaut.,2004

4. Practical uses of liquid methane in rocket engine applications [J];Todd;Acta Astronaut.,2009

5. Use of Extraterrestrial Resources for Human Space Missions to Moon or Mars [M];Rapp,2013
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