发明名称 PROPULSIVE EQUIPMENT AND ROCKET HAVING THE SAME
摘要 PURPOSE: A propulsion engine and a rocket with the same is provided with the improved performance and safety as an insulating part is burst along an interface between first and second insulating members. CONSTITUTION: A propulsion engine(100) comprises a combustion pipe(110), first and second propellants(121,131) and an insulating unit(150). First and second propellants are charged in the combustion pipe. The insulating unit separates the first and second propellants, and insulates a gap between the first and second propellants. The insulating unit is placed between the first and second propellants. The insulating bears the heat and pressure delivered when the first propellant is burned. The insulating unit is burst when the second propellant is ignited.
申请公布号 KR101192203(B1) 申请公布日期 2012.10.17
申请号 KR20120048786 申请日期 2012.05.08
申请人 AGENCY FOR DEFENSE DEVELOPMENT 发明人 LEE, BANG EOP;KIM, WON HOON;KOO, SONG HOE;JUNG, GYOO DONG
分类号 F02K9/10;F02K9/28;F02K9/34 主分类号 F02K9/10
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