磁等离子体动力推力器回顾和认识

Hai Bin Tang; Yi Bai Wang; Yan Ming Wei

doi:10.13675/j.cnki.tjjs.2018.11.001

磁等离子体动力推力器回顾和认识

Translated title of the contribution: Review and Understanding on Magnetoplasmadynamic Thrusters Technology

Hai Bin Tang^*
, Yi Bai Wang
, Yan Ming Wei

^*Corresponding author for this work

School of Astronautics

CAS - Beijing Institute of Control Engineering

Research output: Contribution to journal › Review article › peer-review

8 Scopus citations

Abstract

Due to its high specific impulse,high thrust density and intrinsic capability with on-board nuclear power,the magnetoplasmadynamic thruster (MPDT) has become an attractive option for large delta-v deep space missions in the future. The development history of MPDT technology is reviewed,the thrust generation mechanism and thrust models are summarized. The effects of propellant,operation instabilities,power deposition,electrode structure and cathode erosion etc. on the thruster performance are analyzed. In view of MPDTs technology and future application,some relative knowledge and suggestions are given.

Translated title of the contribution	Review and Understanding on Magnetoplasmadynamic Thrusters Technology
Original language	Chinese (Traditional)
Pages (from-to)	2401-2414
Number of pages	14
Journal	Tuijin Jishu/Journal of Propulsion Technology
Volume	39
Issue number	11
DOIs	https://doi.org/10.13675/j.cnki.tjjs.2018.11.001
State	Published - 1 Nov 2018

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title = "磁等离子体动力推力器回顾和认识",

abstract = "Due to its high specific impulse,high thrust density and intrinsic capability with on-board nuclear power,the magnetoplasmadynamic thruster (MPDT) has become an attractive option for large delta-v deep space missions in the future. The development history of MPDT technology is reviewed,the thrust generation mechanism and thrust models are summarized. The effects of propellant,operation instabilities,power deposition,electrode structure and cathode erosion etc. on the thruster performance are analyzed. In view of MPDTs technology and future application,some relative knowledge and suggestions are given.",

keywords = "Cathode erosion, Electrode structure, Magnetoplasmadynamic thruster, Onset, Power deposition, Propellant, Thrust mechanism",

author = "Tang, \{Hai Bin\} and Wang, \{Yi Bai\} and Wei, \{Yan Ming\}",

year = "2018",

month = nov,

day = "1",

doi = "10.13675/j.cnki.tjjs.2018.11.001",

language = "繁体中文",

volume = "39",

pages = "2401--2414",

journal = "Tuijin Jishu/Journal of Propulsion Technology",

issn = "1001-4055",

publisher = "China Aerospace Science and Industry Corp",

number = "11",

}

TY - JOUR

T1 - 磁等离子体动力推力器回顾和认识

AU - Tang, Hai Bin

AU - Wang, Yi Bai

AU - Wei, Yan Ming

PY - 2018/11/1

Y1 - 2018/11/1

N2 - Due to its high specific impulse,high thrust density and intrinsic capability with on-board nuclear power,the magnetoplasmadynamic thruster (MPDT) has become an attractive option for large delta-v deep space missions in the future. The development history of MPDT technology is reviewed,the thrust generation mechanism and thrust models are summarized. The effects of propellant,operation instabilities,power deposition,electrode structure and cathode erosion etc. on the thruster performance are analyzed. In view of MPDTs technology and future application,some relative knowledge and suggestions are given.

AB - Due to its high specific impulse,high thrust density and intrinsic capability with on-board nuclear power,the magnetoplasmadynamic thruster (MPDT) has become an attractive option for large delta-v deep space missions in the future. The development history of MPDT technology is reviewed,the thrust generation mechanism and thrust models are summarized. The effects of propellant,operation instabilities,power deposition,electrode structure and cathode erosion etc. on the thruster performance are analyzed. In view of MPDTs technology and future application,some relative knowledge and suggestions are given.

KW - Cathode erosion

KW - Electrode structure

KW - Magnetoplasmadynamic thruster

KW - Onset

KW - Power deposition

KW - Propellant

KW - Thrust mechanism

UR - https://www.scopus.com/pages/publications/85059842964

U2 - 10.13675/j.cnki.tjjs.2018.11.001

DO - 10.13675/j.cnki.tjjs.2018.11.001

M3 - 文献综述

AN - SCOPUS:85059842964

SN - 1001-4055

VL - 39

SP - 2401

EP - 2414

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 11

ER -

磁等离子体动力推力器回顾和认识

Abstract

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