载人航天
載人航天
재인항천
MANNED SPACEFLIGHT
2012年
2期
1-6
,共6页
火箭在轨%大尺寸%重负载%交会对接技术
火箭在軌%大呎吋%重負載%交會對接技術
화전재궤%대척촌%중부재%교회대접기술
In-orbit Launch Vehicle%Large Dimension%Heavy Load%Rendezvous and Docking Technology
根据国内外空间交会对接技术的发展现状，以及我国深空探测任务的不断发展，提出研究火箭在轨大尺寸、重负载交会对接技术，满足我国航天事业的未来发展和规划复杂飞行任务的需求。重点对火箭在轨大尺寸、重负载交会对接的关键技术进行了梳理，通过分析认为火箭在轨大尺寸、重负载交会对接技术的研究复杂、难度大、周期长。因此其预研工作的开始已经迫在眉睫。
根據國內外空間交會對接技術的髮展現狀，以及我國深空探測任務的不斷髮展，提齣研究火箭在軌大呎吋、重負載交會對接技術，滿足我國航天事業的未來髮展和規劃複雜飛行任務的需求。重點對火箭在軌大呎吋、重負載交會對接的關鍵技術進行瞭梳理，通過分析認為火箭在軌大呎吋、重負載交會對接技術的研究複雜、難度大、週期長。因此其預研工作的開始已經迫在眉睫。
근거국내외공간교회대접기술적발전현상，이급아국심공탐측임무적불단발전，제출연구화전재궤대척촌、중부재교회대접기술，만족아국항천사업적미래발전화규화복잡비행임무적수구。중점대화전재궤대척촌、중부재교회대접적관건기술진행료소리，통과분석인위화전재궤대척촌、중부재교회대접기술적연구복잡、난도대、주기장。인차기예연공작적개시이경박재미첩。
Based on the current status of rendezvous and docking technology home and abroad, as well as the continuous development of China＇s deep space exploration, the in-orbit launch vehicle rendezvous and docking technology focused on the features of large dimension and heavy load is proposed to meet the future requirements of China＇s aerospace industry. Key technologies of in-orbit launch vehicle rendezvous and docking focused on large dimension and heavy load are analyzed, which include： docking mechanism, attitude control, propulsion system, in-orbit test, simulation technology, and system design. Analysis show that study on the large dimension and heavy load in-orbit launch vehicle rendezvous and docking technology will be very complicated and need a long time to complete, therefore it is extremely urgent to begin the research work in advance.
