Author:
Zeng Linghan,Wu Zhiwen,Sun Guorui,Huang Tiankun,Xie Kan,Wang Ningfei
Funder
National Natural Science Foundation of China
Reference30 articles.
1. Discharge voltage characteristic in ablative pulsed plasma thrusters;Sun;Acta Astronaut.,2019
2. Ignition mechanism in ablative pulsed plasma thrusters with coaxial semiconductor spark plugs;Sun;Acta Astronaut.,2018
3. Overview of major U.S. Industrial programs in electric propulsion;Randolph,1999
4. Development of Russian next-generation ablative pulsed plasma thrusters;Antropov;Acta Astronaut.,2017
5. Correction thruster development based on high-current surface discharge in vacuum;Silnikov;Acta Astronaut.,2015
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