| 高速飞行器头罩分离设计方案研究 |
| |
| 引用本文： | 戈庆明,刘秀春,渠弘毅,吕蒙,刘成国. 高速飞行器头罩分离设计方案研究[J]. 导弹与航天运载技术, 2017, 0(3). DOI: 10.7654/j.issn.1004-7182.20170306 |
| |
| 作者姓名： | 戈庆明 刘秀春 渠弘毅 吕蒙 刘成国 |
| |
| 作者单位： | 北京航天长征飞行器研究所,北京,100076 |
| |
| 摘 要： | 随着飞行器飞行速度的提高,飞行器头部力热环境十分恶劣,需采用头罩分离技术才能保障飞行器精确制导。对高速飞行器的头罩设计及防护设计进行了研究,同时提出了采用导爆索、推冲器的2种头罩分离方案,并进行了抛罩的试验验证和理论仿真计算,试验结果证明了该方法的可行性。
|
| 关 键 词： | 头罩分离技术 导爆索 推冲器 抛罩 |
Research of High-speed Aircraft Shroud Separation Technologies |
| |
| Ge Qing-ming,Liu Xiu-chun,Qu Hong-yi,Lyu Meng,Liu Cheng-guo. Research of High-speed Aircraft Shroud Separation Technologies[J]. Missiles and Space Vehicles, 2017, 0(3). DOI: 10.7654/j.issn.1004-7182.20170306 |
| |
| Authors: | Ge Qing-ming Liu Xiu-chun Qu Hong-yi Lyu Meng Liu Cheng-guo |
| |
| Abstract: | The temperature and thermal stress of the dome surface increased as the rise of the aircraft. Dome protecting is needed for aircraft to target detected accurately. A summary of dome protecting technologies design of high-speed is made in this paper. Two schemes of shroud separation are designed included explosive and thruster. The removal of a dome cover test is done by the explosive cord and the theory simulation is computed which verifies the feasibility of the schemes. |
| |
| Keywords: | Shroud separation technologies Explosive cord Thruster Removal of a dome cover |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
|
