航天推进技术研究院主办
[1]张蒙正,邹 宇.美国典型高超飞行器项目研发及启示[J].火箭推进,2012,38(02):1-8.
ZHANG Meng-zheng,ZOU Yu.Development of American typical hypersonic flight vehicles and its enlightenment[J].Journal of Rocket Propulsion,2012,38(02):1-8.
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ZHANG Meng-zheng,ZOU Yu.Development of American typical hypersonic flight vehicles and its enlightenment[J].Journal of Rocket Propulsion,2012,38(02):1-8.
美国典型高超飞行器项目研发及启示
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
38
期数:
2012年02期
页码:
1-8
栏目:
专论与综述
出版日期:
2012-04-15
- Title:
- Development of American typical hypersonic flight vehicles and its enlightenment
- 文章编号:
- 1672-9374(2012)02-0001-09
- 关键词:
- 高超声速飞行器; 超燃冲压发动机; 火箭基组合循环发动机
- Keywords:
- hypersonic flight vehicle; scramjet; RBCC
- 分类号:
- V43
- 文献标志码:
- A
- 摘要:
- 简要回顾了美国典型高超声速飞行器项目及其动力系统发展的历程，分析了其发展的态势、经验和教训。美国始终将高超声速技术作为航空航天事业发展的重要领域，高超声速飞行器和动力技术方案与国家战略及应用背景密切相关。为了降低技术风险，采取了多方案并行的研发模式。高超声速技术的研发应充分重视顶层设计，注重技术的继承性，发挥不同单位的技术优势，加强基础研究、关键技术攻关和实验设施建设。
- Abstract:
- The development course of American typical hypersonic flight vehicles and their propulsion systems is reviewed. The development trend, experiences and lessons from those typical programs are analyzed. The hypersonic technology is considered as the important development direction of aviation and spaceflight of America. The flight vehicles and propulsion technology have the close relationship with the idiographic application and nation strategic requirement. The development mode coinstantaneous with multi-scheme were adopted to reduce technical risk. The research of hypersonic technology must follow the need of nation strategic development，and focus on the top planning and the technical inheriting. The development of propulsion technology should put great emphasis on the fundamental research, experimental equipment, key technology study and the application of preponderant technique.
参考文献/References:
[1]MCCLINTON C R. Airbreathing hypersonic technology vision vehicle and development dreams, AIAA 99-4978 [R]. USA: AIAA, 1999.
[2]PERKINS H D. Mach 5 to 7 RBCC propulsion system testing at NASA-Lerc HTF, AIAA 97-0565 [R]. USA: AIAA, 1997.
[3]MCCLINTON C R, SITZ J R. Hyper-X: bridge to the hypersonic century[C]// Proceedings of 36th JANNAF CS/PSHS/APS Joint Meeting. Cocoa Beach, FL: APS, 1999: 123-128.
[4]俞刚. 高超声速推进技术的最近动态与分析[C]. 第二届冲压发动机会议, 2007.
[5]KAZMAR R R. Airbreathing hypersonic propulsion at Pratt&Whitney-Overview, AIAA 2005-3256[R]. USA: AIAA, 2005.
[6]于江飞, 刘卫东. 双燃烧室冲压发动机为动力的高超声速飞行器[J]. 导弹与航天运载技术, 2008 (5): 26-30.
[7]温杰. 美国海军的HyFly计划[J]. 飞航导弹. 2008 (12): 12-15.
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备注/Memo
收稿日期：2011-10-13；修回日期：2011-12-06
作者简介：张蒙正（1964—），男，研究员，研究领域为液体火箭发动机
更新日期/Last Update:
1900-01-01