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http://dx.doi.org/10.6108/KSPE.2014.18.1.091

Brief Summary of KSLV-I Upper Stage Kick Motor Development  

Lee, Hanju (Propulsion System Department, Korea Aerospace Research Institute)
Lee, Jung Ho (Propulsion System Department, Korea Aerospace Research Institute)
Oh, Seung Hyub (Propulsion System Department, Korea Aerospace Research Institute)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.18, no.1, 2014 , pp. 91-96 More about this Journal
Abstract
KSLV-I (Korea Space Launch Vehicle-I) upper stage KM (Kick Motor) is a solid propulsion system which consists of igniter, SAD (Safety Arming Device), composite case, and submerged nozzle capable of TVC (Thrust Vector Control) actuation. Each subsystem of KM fulfilled development requirements for achieving a flight mission successfully. We confirmed the successful development of KM from the $3^{rd}$ flight test results of NARO on January 30, 2013. This article deals with the requirements of KM and the results on configuration management, mass variation, thrust axis alignment, and major test results and so on.
Keywords
KSLV-I(Korea Space Launch Vehicle-I); Upper Stage; Kick Motor;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
1 Cho, I.H., Lee, W.B., Kim, Y.M., and Cho, G.R., "Design and Test of KSLV-I Kick Motor," Proceeding of the 2007 KSAS Fall Conference, pp. 1510-1504, 2007.
2 Kim, J.H., GD14530PA00000-0001(B), Korea Aerospace Research Institute, Internal Document, 2006.
3 Chun, Y.D., SP51400PA00000-0001, Korea Aerospace Research Institute, Internal Document, 2004.
4 Lee, H., Jung, D.H., and Oh, S.H., "Configuration Tolerance for KSLV-I Kick Motor System," Aerospace Engineering and Technology, Vol. 10, No. 2, pp. 128-132, 2011.   과학기술학회마을
5 Lee, H., Jung, D.H., and Oh, S.H., "KSLV-I Kick Motor System Thrust Axis Alignment," Aerospace Engineering and Technology, Vol. 9, No. 2, pp. 138-142, 2010.   과학기술학회마을