An Experimental Study on the Regression Rate of the Hybrid Rocket with $GO_2$ /HTPB Propellant Combination
($GO_2$ /HTPB를 사용하는 Hybrid Rocket의 추진제 침투율에 관한 실험적 연구)
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- Journal of the Korean Society of Propulsion Engineers
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- v.1 no.2
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- pp.58-66
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- 1997