01054nam a2200217 c 4500001001300000005001500013008004100028040001100069041001300080052003000093245014900123300003200272545008900304545008600393653011600479700001900595700004800614773013600662900001900798900001900817KSI00007259320040218151255031010s2002    ulka          000   kor    a0110010 akorbeng01a443.105b한569ㅎc19(3)00a인공위성 연료배관의 유압특성 연구=x(A)study on the pressure behavior inside propellant line of satellite/d최진철,e김정수  ap. 207-214:b삽도;c26 cm  a최진철, 스페이스 테크놀로지(주) 우주통신연구소bjcchoi@stc21.com  a김정수, 한국항공우주연구원 위성제어연구그룹bjskim@kari.re.kr  aSatelliteaPropulsion systemaPropellantaPressure dropaUnsteady flowaMOCa인공위성a연료배관a유압1 a최진철4aut1 a김정수,g金楨洙,d1961-0KAC2017381930 t韓國宇宙科學會誌.d韓國宇宙科學會.g19卷 3號(2002년 9월), p. 207-214q19:3<207w(011001)KSE199500817,x1225-052X10aChoi, Jin-Chul10aKim, Jeong-Soo