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기술보고서

기술보고서 게시판 내용
타이틀	Theoretical Performance of Rocket Engine for Liquid Oxygen/High Density Hydrocarbon/Metal System
저자	Kazuo SATO, Akio MORO, Nobuyuki YATSUYANAGI, Hiroshi SAKAMOTO
Keyword	Propulsion; Liquid rocket; Dual fuel; Metalized fuel
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltm00659.pdf?id=NALTM0000659
보고서번호	NAL TM-659
발행년도	1993.8
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	The theoretical performance of a rocket engine using liquid oxygen (LO2) /hydrocarbon (HC) /metal propellant was calculated by one-dimensional chemical equilibrium flow method. The hydrocarbon fuel used was the petroleum-derived RJ-1J with a density of 851 kg/m3 at 25℃. Beryllium, boron, aluminum and magnesium were selected as the additive metals to the LO2/HC propellant to improve the specific impulse and increase bulk density of the propellat. The results indicate t