01222cam a22003251i 4500001001300000005001500013007000300028008004100031040003200072041001300104049001800117052001800135056001100153082001400164100003600178245014800214264003800362300004400400336002600444337002900470338002700499500002700526502010300553504003200656546003400688653011400722900001700836900001900853900002400872KDM20185027020200717165613ta180105s2018    ulka     m AQ 000c  eng    a211046c011012d011001erda0 aengbkor0 lWM905543fWDP02a621.8b18-258  a5502601a621.82231 a배지열,d1988-0KAC20162953810aThermochemical analysis for design of composite rocket nozzle =x열화학반응 분석을 통한 복합재 로켓 노즐 설계 /dJi-yeul Bae 1aSeoul :bYonsei University,c2018  axi, 146 pages :billustrations ;c26 cm  atextbtxt2rdacontent  aunmediatedbnc2rdamedia  avolumebnc2rdacarrier  aAdviser: Hyung Hee Cho1 aThesis(Ph.D.) --bGraduate School, Yonsei University,cDepartment of Mechanical Engineering,d2018  aBibliography: pages 140-144  aIn English; summary in Korean  a로켓노즐a삭마a열분해a내열재a숯층a열분해가스a연소가스a열물질상사a열응답10aBae, Ji-Yeul10aCho, Hyung Hee10aBae, Jiyeul,d1988-