Advanced Search
TANG Zhangyang, ZHOU Cheng, HAN Dong, MA Xue, CHEN Tao. Study on High Power All-Electric Propulsion System for Spacecraft Orbit TransferJ. Journal of Deep Space Exploration, 2018, 5(4): 367-373. DOI: 10.15982/j.issn.2095-7777.2018.04.007
Citation: TANG Zhangyang, ZHOU Cheng, HAN Dong, MA Xue, CHEN Tao. Study on High Power All-Electric Propulsion System for Spacecraft Orbit TransferJ. Journal of Deep Space Exploration, 2018, 5(4): 367-373. DOI: 10.15982/j.issn.2095-7777.2018.04.007

Study on High Power All-Electric Propulsion System for Spacecraft Orbit Transfer

  • Compared with chemical propulsion,the application electric propulsion system in spacecraft can save the amount of propellant,which is able to significantly reduce the launch mass or allow more payloads to the target. In this paper,the research on high power electric thrusters in the world is investigated. An electric propulsion systemis designed for the near-earth spacecraft orbit transfer. Several schemes are compared with different thruster performances. At last,the suggestions are proposed for developing high power electric thruster and propulsion system in China.
  • loading

Catalog

    Turn off MathJax
    Article Contents

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return
    Baidu
    map