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Journal of the Korea Institute of Military Science and Technology 2004;7(2):126-135.
Firing Test of KSR-III Rocket Propulsion System
Sun-Il Kang, Oh-Sung Kwon, Jung-Ho Lee, Young-Han Kim, Seong-Up Ha, Kwang-Rae Cho
KARI
KSR-III 로켓 추진기관 연소시험
강선일, 권오성, 이정호, 김영한, 하성업, 조광래
한국항공우주연구원
Abstract
The KSR-III rocket developed by KARI is the first rocket vehicle which is adopting the liquid propellant rocket engine system in Korea and its flight test was successfully done last year, KSR-III is a sounding rocket class launch vehicle, but there is a sense to accomplish design, manufacture, performance test and finally its flight test by domestic technology. In this paper, the authors are intended to introduce the multi-purpose test facility(PTA-II Test Facility) which is constructed for the variety of tests on KSR-III feeding system(single component tests, verification tests, cold flow tests and combustion tests) and its firing test results.
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