01163nam a2200217 c 4500001001300000005001500013008004100028040001100069041001300080052002900093245016500122300002200287545008500309545006500394653026500459700001900724700003600743773013100779900001800910900001700928KSI00091443020131203090616131122s2013    tjk           000   kor    a0110010 akorbeng01a572.05b한626ㅎc17(3)00aRBCC엔진을 적용한 재사용발사체의 중량저감효과 =xWeight reduction of the reusable launch vehicles using RBCC engines /d강상훈,e이수용  ap. 56-66 ;c26 cm  a강상훈, 한국항공우주연구원 미래로켓연구팀baeroksh@kari.re.kr  a이수용, 한국항공우주연구원 미래로켓연구팀  a재사용발사체a로켓복합사이클 엔진a수직이륙/수평착륙a2단 발사형a스크램제트a램제트aReusable launch vehicleaRocket based combined cycle engineaVertical take off and horizontal landingaTwo stage to orbitaScramjetaRamjet1 a강상훈4aut1 a이수용,d1957-0KAC2018443570 t한국추진공학회지.d韓國推進工學會.gVol.17 No.3(2013 June), p. 56-66q17:3<56w(011001)KSE199902389,x1226-602710aKang, Sanghun10aLee, Sooyong