Thrust and efficiency of the K-III MPD thruster-Reference-Cited by-同舟云学术

Thrust and efficiency of the K-III MPD thruster

Published:1984-09 Issue:5 Volume:21 Page:481-487
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Yoshikawa Takao¹,Kagaya Yoichi¹,Kuriki Kyoichi²

Affiliation:

1. Osaka University, Osaka, Japan

2. Institute of Space and Astronautical Science, Tokyo, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.25683

Reference19 articles.

1. ^alliaris, A.C. John, R.R., Garrison, R.L., and Libby, D.R. "Quasi-Steady MPD Propulsion at High Power," Final Tech. Report AVSD-0146-71-RR, AVCO Corp.NASA CR111872, Feb. 1971.

2. 2King, D.Q., Smith, W.W., John, R.R., and Clark, K.E. "Effect of Thrust Chamber Configuration on MPD Arcjet Performance," AIAA Paper 79-2051,1979.

3. Flowfield Characteristics and Perf ormance Limitations of Quasi-Steady Magnetoplasmadynamic Accelerators

4. Thrust Measurement of KIII MPD Arcjet

5. Transitional Behavior of MPD Arcjet Operation

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