Thrust Measurement of a Cold Gas Thruster for KSLV-I under Vacuum Conditions-Reference-Cited by-同舟云学术

Thrust Measurement of a Cold Gas Thruster for KSLV-I under Vacuum Conditions

Published:2015 Issue:2 Volume:58 Page:108-109
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:

JEON Sangwoon¹,JUNG Seul²,KIM Jihun³,KIM Joonyun⁴

Affiliation:

1. Launcher Systems Development Team, Korea Aerospace Research Institute

2. Department of Mechatronics Engineering, Chungnam National University

3. Launcher Stage Engineering Team, Korea Aerospace Research Institute

4. Launcher Electronics Team, Korea Aerospace Research Institute

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/58/2/58_T-13-54/_pdf

Reference4 articles.

1. 1) KARI: Research and Development of KSLV-I, MSIP, 2013.

2. 2) Adler, S., Warshavsky, A., and Peretz, A.: Low-cost Cold-gas Reaction Control System for Slohsat FLEVO Small Satellite, J. Spacecraft Rocket, 42, 2 (2005), pp. 345–351.

3. 3) Stone, W. C.: Fast Variable-amplitude Cold Gas Thruster, J. Spacecraft Rockets, 32, 2 (1995), pp. 335–343.

4. 4) Jeon, S.-W. and Jung, S.: Hardware in the Loop Simulation for the Reaction Control System using PWM-based Limit Cycle Analysis, IEEE Trans. Control Syst. Technol., 20, 2 (2012), pp. 538–545.

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