首页 | 本学科首页   官方微博 | 高级检索  
     检索      

新一代多用途载人飞船概念研究
引用本文:杨雷,张柏楠,郭斌,左光,石泳,黄震.新一代多用途载人飞船概念研究[J].航空学报,2015,36(3):703-713.
作者姓名:杨雷  张柏楠  郭斌  左光  石泳  黄震
作者单位:中国空间技术研究院 载人航天总体部, 北京 100094
摘    要:在"神舟"载人飞船进入成熟稳定期后,中国有必要尽早启动新一代多用途载人飞船的论证和研制。本文对国外新一代载人飞船的技术方案特点、新的设计理念及发展现状进行了分析,从适应多任务、降低运营成本、钝头体气动外形、更高安全可靠性以及新型轻质材料使用等多个方面总结了国外新一代载人飞船的技术发展趋势。初步分析了中国发展新一代载人飞船的近地轨道、载人登月、载人登小行星、载人登火星等任务需求,基本确定了新一代飞船的总体性能参数,并在此基础上梳理了新一代载人飞船技术途径,初步提出了两种方案设想,为中国新一代载人飞船的研制提供参考。

关 键 词:新一代载人飞船  多用途  逃逸  再入  任务需求  总体方案  
收稿时间:2014-08-13;

Concept definition of new-generation multi-purpose manned spacecraft
YANG Lei , ZHANG Bainan , GUO Bin , ZUO Guang , SHI Yong , HUANG Zhen.Concept definition of new-generation multi-purpose manned spacecraft[J].Acta Aeronautica et Astronautica Sinica,2015,36(3):703-713.
Authors:YANG Lei  ZHANG Bainan  GUO Bin  ZUO Guang  SHI Yong  HUANG Zhen
Institution:Institution of Manned Spacecraft System Engineering, China Academy of Space Technology, Beijing 100094, China
Abstract:With the Shenzhou spacecraft entering into the stage of maturity, it is of necessity to launch the research and development of a new-generation multi-purpose manned spacecraft. In this paper, we firstly generalize the technological characteristics, the design concept and the status quo of the foreign new-generation manned spacecraft. Based on this, we summarize their technological trend, i.e., multi-task adaption, cost reduction, bluntbody aerodynamic configuration, high safety reliability and new lightweight materials. Then, we primarily analyze the task requirements of China''s new-generation manned spacecraft, including low earth orbit flight mission, as well as manned flights to the Moon, the asteroid and the Mars. We basically set the parameters of the overall performance. Finally, we sort out the technological approaches of it and propose two design schemes, which could provide some reference for the research of China''s new-generation manned spacecraft.
Keywords:new-generation manned spacecraft  multi-purpose  launch abort  reentry  task requirement  design scheme
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号