Performance Evaluation of Combustion-controllable 0.1-N-Class Solid Propellant Microthrusters Using Laser Heating-Reference-Cited by-同舟云学术

Performance Evaluation of Combustion-controllable 0.1-N-Class Solid Propellant Microthrusters Using Laser Heating

Published:2021 Issue:2 Volume:64 Page:65-70
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

HARAGUCHI Daichi¹,ISAKARI Shota²,YANO Yasuyuki³,KAKAMI Akira⁴

Affiliation:

1. Department of Engineering, University of Miyazaki

2. Department of Mechanical Systems Engineering, University of Miyazaki

3. Technical Center, University of Miyazaki

4. Department of Aeronautics and Astronautics, Tokyo Metropolitan University

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/64/2/64_T-19-37/_pdf

Reference9 articles.

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2. 2) Doncaster, B., Williams, C., and Shulman, J.: 2017 Nano/Microsatellite Market Forecast, Small Satellite Report, SpaceWorks Enterprises, Inc., 2017.

3. 3) Asakawa, J., Koizumi, H., Kojima, S., Nakano, M., and Komurasaki, K.: Laser-Ignited Micro-Motor Using Multiple Stacked Solid Propellant Pellets, J. Propul. Power, 35, 1 (2019), pp. 41–53.

4. 4) Kakami, A., Hiyamizu, R., Shuzenji, K., and Tachibana, T.: Laser-Assisted Combustion of Solid Propellants at Low Pressures, J. Propul. Power, 24, 6 (2008), pp. 1350–1360.

5. 5) Kakami, A., Hamada, T., Shimoda, M., and Tachibana, T.: Throttleable Solid Propellant Microthruster Using Laser-assisted Combustion, Proc. of 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, San Jose, AIAA-2013-4078, 2013.