QUASI-STEADY MAGNETOPLASMADYNAMIC THRUSTER WITH APPLIED MAGNETIC-FIELDS FOR NEAR-EARTH MISSIONS

被引：13

作者：

TAHARA, H

KAGAYA, Y

YOSHIKAWA, T

机构：

[1] Osaka Univ, Japan

来源：

JOURNAL OF PROPULSION AND POWER | 1989年 / 5卷 / 06期

关键词：

10;

D O I：

10.2514/3.23210

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：713 / 717

页数：5

共 10 条

[1]

Kelly, 1968, CRITICAL REV MAGNETO

[2] PERFORMANCE CHARACTERISTICS OF A MAGNETIC ANNULAR ARC [J].

PATRICK, RM ;

SCHNEIDE.AM .

AIAA JOURNAL, 1966, 4 (02) :283-&

[3]

SAKIYAMA M, 1987, AIAA871045 PAP

[4]

TAHARA H, 1985, AIAA852001 PAP

[5] MPD THRUSTER PERFORMANCE WITH VARIOUS PROPELLANTS [J].

UEMATSU, K ;

MORIMOTO, S ;

KURIKI, K .

JOURNAL OF SPACECRAFT AND ROCKETS, 1985, 22 (04) :412-416

[6]

UEMATSU K, 1987, AIAA871023 PAP

[7]

UEMATSU K, 1984, 17TH INT EL PROP C T, P79

[8] THRUST AND EFFICIENCY OF THE K-III MPD THRUSTER [J].

YOSHIKAWA, T ;

KAGAYA, Y ;

KURIKI, K .

JOURNAL OF SPACECRAFT AND ROCKETS, 1984, 21 (05) :481-487

[9]

YOSHIKAWA T, 1984, 17TH P JSASS AIAA DG, P396

[10]

YOSHIKAWA T, 1985, AIAA852003 PAP

← 1 →