| 两级入轨完全重复使用运载火箭的方案分析与轨道仿真计算 |
| |
| 引用本文： | 果琳丽,刘竹生,朱永贵,余梦伦,唐一华. 两级入轨完全重复使用运载火箭的方案分析与轨道仿真计算[J]. 导弹与航天运载技术, 1999, 0(6): 1-9 |
| |
| 作者姓名： | 果琳丽 刘竹生 朱永贵 余梦伦 唐一华 |
| |
| 作者单位： | 北京宇航系统工程设计部,北京,100076 |
| |
| 摘 要： | 运载火箭实现重复使用是未来运载火箭的发展趋势之一，本文首先简单地介绍了肖妆国外重使用技术的发展状况，然后根据我国的国情提出了一种两级入轨可一重复使用方法，接着对该方案的返回轨道特性进行了研究，通过分析仿真计算结果，论证了火箭全部回收的可行性，最后提出了谷进一步深入研究此方案所需做的关键技术研究工作。
|
| 关 键 词： | 重复使用运载火箭 单级入轨运载器 再入弹道 |
| 修稿时间： | 1999-04-20 |
Concept Research of Two Stage to Orbit and Fully Reusable Launch Vehicle |
| |
| Guo Linli,Liu Zhusheng,Zhu Yonggui,Yu Mongleng,Tang Yiha. Concept Research of Two Stage to Orbit and Fully Reusable Launch Vehicle[J]. Missiles and Space Vehicles, 1999, 0(6): 1-9 |
| |
| Authors: | Guo Linli Liu Zhusheng Zhu Yonggui Yu Mongleng Tang Yiha |
| |
| Abstract: | Reusable launch vehicle is one of the development trends of future launch vehicle.Firstly,the development status of foreign reusable launch vehicle technology is briefly introduced.Then,a concept of two stage to orbit and fully reusable launch vehicle is put forward.The return trajectory characteristics of the concept is analysed and the reasibility of full rocket recoverability is validated by analysing the simulation results.Lastly ,the key technology items which should be studied are pointed out. |
| |
| Keywords: | Recoverable launch vehicle Single stage to orbit vehicle Reentry trajectory. |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
|
