论文部分内容阅读
针对基于在轨加注站模式的空间运输系统,分析了其执行地球空间任务、载人月球探测任务、载人小行星探测任务和载人火星探测任务时采用的不同空间运输系统组合,对比了反推减速和气动减速两种方式,得到了具体的加注站及其空间运输系统的规模和数量需求。结果表明基于在轨加注站的整个空间运输系统规模和在轨加注规模有限,数量可控,可实现性强,利用两个加注站和有限数量的空间转移运载器就能满足多种空间探测任务的需求。
Aiming at the space transportation system based on the in-orbit filling station mode, this paper analyzes the different space transportation system combinations used in the mission of carrying out the earth space, the manned lunar exploration mission, the manned asteroid exploration mission and the manned Mars exploration mission. Thrust reduction and pneumatic deceleration in two ways, the specific filling station and its space transportation system, the size and quantity requirements. The results show that the total space transportation system based on on-orbit filling stations is limited in scale and in-orbit-on-a-scale and controllable in number and achievable, with two filling stations and a limited number of space transfer vehicles Space exploration mission needs.