Impulse and electric charge characteristics of chemical propellant under pulsed laser irradiation-Reference-Cited by-同舟云学术

Impulse and electric charge characteristics of chemical propellant under pulsed laser irradiation

Published:2021-10 Issue: Volume:192 Page:110419
ISSN:0042-207X
Container-title:Vacuum
language:en
Short-container-title:Vacuum

Author:

Duan Buren,Zhang Haonan,Hua Zuohao,Wu Lizhi^ORCID,Bao Zijing,Guo Ning,Ye Yinghua,Shen Ruiqi

Funder

Fundamental Research Funds for the Central Universities

Shanghai Aerospace Science and Technology Innovation Foundation

Publisher

Elsevier BV

Subject

Surfaces, Coatings and Films,Condensed Matter Physics,Instrumentation

Reference45 articles.

1. Smaller Satellites: Bigger Business Bigger Business: Concepts, Applications and Markets for Micro/Nanosatellites in a New Information World;Rycroft,2002

2. Small Satellites: Past, Present, and Future;Helvajian,2008

3. Small satellite market observations;Elizabeth,2015

4. Total impulse improvement of coaxial pulsed plasma thruster for small satellite;Aoyagi;Vacuum,2008

5. Design and performance of liquid propellant pulsed plasma thruster;Kakami;Vacuum,2004

Cited by 13 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. MOFs for Ultrahigh Efficiency Pulsed Laser Micropropulsion;Advanced Materials;2023-11-27

2. Study on the ablation of a pulsed plasma thruster with a non-volatile liquid propellant;Vacuum;2023-10

3. Experimental Investigation on Plume Characteristics of PTFE-Filled Carbon, Graphite, Graphene for Laser-Assisted Pulsed Plasma Thruster;Applied Sciences;2023-08-16

4. Ignition and Extinction Characteristics of Electrically Controlled Solid Propellants;Journal of Propulsion and Power;2023-05

5. Study of a low-power micro coaxial pulsed plasma thruster with axial applied magnetic field;Vacuum;2023-04