|Table of Contents|

Development trends and directions of liquid ramjet/scramjet technology(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2011年04期
Page:
12-17
Research Field:
专论与综述
Publishing date:

Info

Title:
Development trends and directions of liquid ramjet/scramjet technology
Author(s):
MA Jie LIANG Jun-long
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
Keywords:
supersonic cruise missile aircraft liquid ramjet technical direction research progress
PACS:
V439-34
DOI:
-
Abstract:
The liquid ramjet engine is an ideal propulsion device for supersonic cruise missiles and unmanned air vehicles. All the military powers are actively developing the ramjet/scramjet technology. Through reviewing and expounding on the development process of liquid ramjet/scramjet abroad, the development trends and directions of ramjet/scramjet technology were sorted out.

References:

[1] 郑日恒. 法国冲压发动机研究进展[J]. 航天制造技术, 2006 (2): 6-10, 22.
[2]CALZONE R F. Developments in missile ramjet propulsion, AD-A322627 [R]. USA: AD, 1996.
[3]MINARD J P, HALLAIS M, FALEMPIN F. Low cost ramjet technology for tactical missile application, AIAA 2002-3765 [R]. USA: AIAA, 2002.
[4]FRY Ronald S. A century of ramjet propulsion technology evolution[J]. Journal of Propulsion and Power, 2004, 20(1): 27-58.
[5]过武宏, 袁彩锦, 朱汉雨. 巡航导弹潜艇发展历程与趋势[J]. 飞航导弹, 2009(7): 29-32+36.
[6]汪玉, 姚耀中. 世界海军潜艇[M]. 北京: 国防工业出版社, 2006.
[7]靳涛. 俄海军巡航导弹潜艇发展历程[J]. 海事大观, 2005(4): 40-45.
[8]高建军. 未来空面制导武器发展趋势[J]. 飞航导弹, 2009(6): 16-19.
[9]张佐成, 钟建业. 印度的导弹武器装备[J]. 飞航导弹, 2006 (7): 7-16.
[10]曹临. 空地巡航导弹: 防区外攻击的主力[J]. 兵器知识, 2005 (2): 49-53.
[11]王蒙, 张纯学. 空对空武器发展概况[J]. 飞航导弹, 2006(5): 3-5.
[12]孟宇鹏, 郑日恒. 超声速进气道与飞航导弹一体化发展概述[J]. 飞航导弹, 2008 (1): 47-51.
[13]毕士冠. 国外超声速巡航导弹发展战略与技术途径讨论(上)[J]. 飞航导弹, 2007(1): 1-9.
[14]毕士冠. 国外超声速巡航导弹发展战略与技术途径讨论(下)[J]. 飞航导弹, 2007(2): 1-8, 21.
[15]魏毅寅, 刘鹏, 张冬青, 等. 国外高超声速技术发展及飞行试验情况分析[J]. 飞航导弹,2010(5): 2-5.
[16]HANK Joseph M, MURPHY James S, MUTZMAN Richard C. The X-51A scramjet engine flight demonstration program, AIAA 2008-2540 [R]. USA: AIAA, 2008.
[17]曾慧, 白菡尘, 朱涛. X-51A超燃冲压发动机及飞行验证计划[J]. 导弹与航天运载技术, 2010(1): 57-61.
[18]朱爱平, 叶蕾. 法俄联合进行Kholod双模态冲压发动机飞行试验分析[J]. 飞航导弹, 2010(2): 64-69.
[19]FALEMPIN F,SERRE L. LEA flight test program: status in 2004, AIAA 2004-3344 [R]. USA: AIAA, 2004.
[20]张炜, 朱慧, 方丁酉, 等. 冲压发动机发展现状及其关键技术[J]. 固体火箭技术, 1998, 21(3): 24-30.
[21]BURNERS R, LEE M J, MCMANIGAL J. Thermal management in hypersonic vehicles: characterization of phase change materials, AIAA 2001-3974[R]. USA: AIAA, 2001.

Memo

Memo:
-
Last Update: 1900-01-01