1、 ?ZC# 1o/ f Z f(S S/v, , 410073)K1 对国内外冲压推进技术的发展现状进行了对比分析,论证了我国加快开展冲压发动机及相关技术研究的必要性b分析了冲压发动机驱动的导弹总体技术a进气道/转弯方式/冲压补燃室(无壅塞式应同时考虑燃气发生器)一体化设计a贫氧推进剂a燃气发生器a助推器及转级等方面的关键技术b5M 冲压火箭发动机 导弹 冲压喷气发动机导弹1 -“5 r/ af F 8“d#Q“d,l ? 3i ? 4 1 pb “ - 3. 5 24. 48 TA8 ?/ T S5 b b AAAM 370 3 30. 58 T%8p ? S t9SCM b8 Tp ?a
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4、s bZS 6 b, l? Tb S= ? ) V9X|bb |w ?s 7 ! !9Z;9F 8, H 5b i w !99F E ;71 w s 5 byN 7S |w i 8 T !9Z b ? z%8pw i ? iB8)8 Tp ?( IRR) 1+b8 Tp ?w T ,| ,7 O i 5 =FB V 3 i bB%8p ?1 6850 7 840N#s/ kgW, %8p ?7, ? 1Bt;M1/, V)28)1998 M9%8p/ 21 %8p ? ? Bt, ? 1 A8 ?b5N,%8 ? ? ! HW , + YZ 1A8 ?b%8 ?1 A8 ?%8p ? ? W,
5、 1 BV9 800N#s/ kg,1A8 ?1Btb=Q i = b V9F?1 ,4K;%8 ? ! “d V v41 b ?,A8 ? KL,M1/%8p ?%8 ? bA8 ? e“di, P vv9Fb%8 ?e, 9 K, i = 0/ 9F1y B, =d + i 1 p, y Bb%8p ? M) ) ? 3 i 9F1y , 6 “d99F b5 %8p ?Z1o/ V s V A,%8p ?/ S?Z ?/ VBobS S= ?/ F ?Zv t ,S M%8p ?Z , 7Z%8p ?M1/ ,* !9aS1 !9 ? zT / %!bT ,S%8p ?V /+Z ?Z:
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7、; w4 ?b w4 .ft .t?W ,:t, 19926 ,o. ? %8w44 ?.w/ , 1992, ( 5) : 687 o, . 0V w4 s+Y.a(s) , 1997, ( 1)Developmentof RamjetandDuctedRocketEnginesZhang Wei Zhu Hui Fang Dingyou Zhang Weihua( National University of Defense Technology, Changsha, 410073)Abstract The development state of the ramjet and ducte
8、d rocketis in this field was reviewed. T he key tech-niques in the development of solid ducted rocket, such as, the system design method, inlet/ turn mode/ ram-combustor uniform design techniques, fue-l rich propellant, gas generator, air ducted combustion chamber,booster etc are analyzedSubjectTerms Ducted rocket engine Missile Ramjet missile)30)1998 M9%8p/ 21
