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http://dx.doi.org/10.5139/JKSAS.2004.32.7.091

Range Safety System Operation in KSR-III Flight Test  

Ko, Jeong-Hwan (한국항공우주연구원 우주발사체사업단)
Kim, Jeong-Rae (한국항공우주연구원 우주발사체사업단, 한국항공대학교 항공우주 및 기계공학부)
Park, Jeong-Joo (한국항공우주연구원 우주발사체사업단)
Bang, Hee-Jin (국방과학연구소 종합시험단)
Choi, Dong-Min (국방과학연구소 종합시험단)
Song, Sang-Sup (국방과학연구소 종합시험단)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.32, no.7, 2004 , pp. 91-97 More about this Journal
Abstract
The first Korean liquid propellant rocket KSR-III successfully finished its flight test on Nov. 28, 2002. Herein, we summarize the results of range safety system operation which is employed for the first time in flight tests of rockets developed by Korea Aerospace Research Institute(KARI). During the flight, safety-critical flight data including instantaneous impact points are monitored in realtime by range safety officers utilizing Range Safety Display Systems. The recorded screen of the display system is presented for the explanation of safety operation. In addition, comparisons are made between onboard navigation system based and radar based results in calculating instantaneous impact points, and also errors from the finally recorded impact point are described.
Keywords
KSR-III; Flight Test; Range Safety; Flight Termination; Instantaneous Impact Point;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
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