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A model for macro-performances applied to low power coaxial pulsed plasma thrusters

  • Published:2020-05 Issue: Volume:170 Page:154-162
  • ISSN:0094-5765
  • Container-title:Acta Astronautica
  • language:en
  • Short-container-title:Acta Astronautica

Author:

Li Hang,Wu Zhiwen,Sun Guorui,Zhu Kangwu,Huang Tiankun,Liu Xiangyang,Ling William Yeong Liang,Wang Ningfei

Funder

National Natural Science Foundation of China

Natural Science Foundation of Shanghai

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. Discharge voltage characteristic in ablative pulsed plasma thrusters;Sun;Aerospace Sci. Techonol.,2019

2. Discharge reliability in ablative pulsed plasma thrusters;Wu;Acta Astronaut.,2017

3. Optimization of the energy distribution in ablative pulsed plasma thrusters;Wu;AIAA J.,2018

4. Results of the qualification test campaign of a pulsed plasma thruster for cubesat propulsion (PPTCUP);Ciaralli;Acta Astronaut.,2016

5. CubeSat evolution: analyzing CubeSat capabilities for conducting science missions;Poghosyan;Prog. Aerosp. Sci.,2017
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