A method for evaluating the thrust of a space propulsion device with wide range time variations using a disturbance observer-Reference-Cited by-同舟云学术

A method for evaluating the thrust of a space propulsion device with wide range time variations using a disturbance observer

Published:2015-11 Issue:11 Volume:86 Page:115114
ISSN:0034-6748
Container-title:Review of Scientific Instruments
language:en
Short-container-title:Rev. Sci. Instrum.

Author:

Kakami Akira¹,Muto Takuya²,Yano Yasuyuki³,Tachibana Takeshi⁴

Affiliation:

1. Department of Mechanical Design Systems Engineering, University of Miyazaki, 1-1 Gakuenkibanadai-nishi, Miyazaki 889-2192, Japan

2. Department of Mechanical Systems Engineering, University of Miyazaki, 1-1 Gakuenkibanadai-nishi, Miyazaki 889-2192, Japan

3. Faculty of Engineering, University of Miyazaki, 1-1 Gakuenkibanadai-nishi, Miyazaki 889-2192, Japan

4. Department of Mechanical Engineering, Kyushu Institute of Technology, 1-1 Sensui-cho, Tobata, Kitakyushu, Fukuoka 884-8550, Japan

Publisher

AIP Publishing

Subject

Instrumentation

Reference21 articles.

1. K. W. Stark, T. Dennis, D. McHugh, and T. Williams, “Design and development of a micropound extended range thrust stand (merts),” Technical Report NASA TN D-7029 (National Aeronautics and Space Administration, 1971).

2. H. Koizumi, A. Kakami, K. Komurasaki, and Y. Arakawa, in Selected Paper of 23rd International Symposium on Space Technology and Science (Japan Society for Aeronautical and Space Sciences (JSASS), 2002), p. 295.

3. T. W. Haag, in Proceedings of The 31st Joint Propulsion Conference & Exhibit, 1995.

4. Development of a Specific Impulse Balance for Capillary Discharge Pulsed Plasma Thrusters

5. Torsional thrust balance measurement system development for testing reaction control thrusters

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