Browse > Article
http://dx.doi.org/10.5139/JKSAS.2003.31.1.104

Thruster Attitude Control System for the Ksr-3  

Jeong,Ho-Rak (한국항공우주연구원)
Jeon,Sang-Un (한국항공우주연구원)
Choe,Hyeong-Don (한국항공우주연구원)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.31, no.1, 2003 , pp. 104-112 More about this Journal
Abstract
This paper introduces a thruster attitude control system for the KSR-III and addresses system configuration, design condition for several components and development systems. These systems were confirmed through environmental tests, compatibility tests with other sub-systems and are planned to launch by this year. After the launch test, it can be redesigned for optimal systems using post-analysis.
Keywords
Attitude Control; Thruster; Regulator;
Citations & Related Records
연도 인용수 순위
  • Reference
1 채연석 외, "3단형 과학로켓 개발사업(I)", 과학기술부, 1998
2 채연석 외, “3단형 과학로켓 개발사업 (II)", 과학기술부, 1999
3 채연석 외, “3단형 과학로켓 개발사업 (III)", 과학기술부, 2000
4 채연석 외, “3단형 과학로켓 개발사업 (IV)", 과학기술부, 2001
5 Walker, R E., Stone, A. R., and Shandor, M., "Secondary Gas Injection in a Conical Rocket Nozzle," AIAA Journal, Vol. 1, Feb. 1963, pp.334-338.   DOI
6 Merer, J. W. and Jenkins, C. A., "Attitude Control Systems for Sounding Rockets," AIAA 2nd Sounding Rocket Technology Conference, Dec., 1970
7 Windsor, R., "Goddard Space Flight Center Sounding Rocket Facilities at White Sands Missile Range," AIAA 4th Sounding Rocket Technology Conference, Boston, Massachusettes, June 23-25, 1976
8 Olney, D., "Development of a Magnetic Acquisition and Attitude Control System for Spinning Rocket Payloads," AIAA 6th Sounding Rocket Technology Conference, Orlando, Florida, October 26-28, 1982