Prospects of use of electromagnetic railgun as plasma thruster for spacecrafts-Reference-Cited by-同舟云学术

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Prospects of use of electromagnetic railgun as plasma thruster for spacecrafts

Published:2018-09 Issue: Volume:150 Page:92-96
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Poniaev S.A.,Reznikov B.I.,Kurakin R.O.,Popov P.A.,Sedov A.I.,Shustrov Y.A.,Zhukov B.G.

Funder

RFBR

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference20 articles.

1. Plasma thrusters;Morozov,2003

2. Propulsion for CubeSats;Lemmer;Acta Astronaut.,2017

3. Thrust efficiency optimization of the pulsed plasma thruster SIMP-LEX;Nawaz;Acta Astronaut.,2010

4. Pulsed plasma thruster;Burton;J. Propul. Power,1998

5. The analysis of high amplitude of potential oscillations near the hollow cathode of ion thruster;Qin;Acta Astronaut.,2017

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1. Effect of driving current profile on acceleration efficiency of electromagnetic railgun;AIP Advances;2024-08-01

2. Modular electromagnetic railgun accelerator for high velocity impact studies;Review of Scientific Instruments;2022-12-01

3. About the Limitation for the Plasma Motion Velocity in Electrodynamic Accelerator;Plasma Physics Reports;2022-03

4. Infiltrated tungsten-copper composite reinforced with short tungsten fibers;Vacuum;2020-03

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