节点文献
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
Concept Research of Two Stage to Orbit and Fully Reusable Launch Vehicle
【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当前国外重复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完全重复使用的方案,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,最后提出了欲进一步深入研究此方案所需做的关键技术研究工作。
【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.
【关键词】 重复使用运载火箭;
单级入轨运载器;
再入弹道;
【Key words】 Recoverable launch vehicle; Single stage to orbit vehicle; Reentry trajectory.;
【Key words】 Recoverable launch vehicle; Single stage to orbit vehicle; Reentry trajectory.;
- 【文献出处】 导弹与航天运载技术 ,MISSILES AND SPACE VEHICLES , 编辑部邮箱 ,1999年06期
- 【分类号】V475.1
- 【被引频次】8
- 【下载频次】458