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NTIS 바로가기한국추진공학회지 = Journal of the Korean Society of Propulsion Engineers, v.11 no.2 = no.39, 2007년, pp.26 - 36
황기영 (국방과학연구소 추진기관부) , 임유진 (국방과학연구소 추진기관부) , 함희철 (국방과학연구소 추진기관부) , 강윤구 (국방과학연구소 추진기관부) , 배주찬 (국방과학연구소 추진기관부)
The thermal response characteristics of nozzle liner for a solid rocket motor applying highly aluminized PCP or HTPB propellant with slotted tube grain have been investigated. The SEM photographs of aluminum oxide particles taken from nozzle liner show that the PCP propellant with the finer and less...
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