干旱区生态环境知识资源中心(Arid): Solar Electric Propulsion Vehicle Design Study for Cargo Transfer to Earth-moon L1

Arid

报告编号	NASA/TM-2002-211970, E-13613, NAS 1.15:211970, AIAA Paper 2002-3971
来源ID	NTRS_Document_ID: 20020085156
	Solar Electric Propulsion Vehicle Design Study for Cargo Transfer to Earth-moon L1
	Sarver-Verhey, Timothy R.; Kerslake, Thomas W.; Rawlin, Vincent K.; Falck, Robert D.; Dudzinski, Leonard J.; Oleson, Steven R.
英文摘要	A design study for a cargo transfer vehicle using solar electric propulsion was performed for NASA's Revolutionary Aerospace Systems Concepts program. Targeted for 2016, the solar electric propulsion (SEP) transfer vehicle is required to deliver a propellant supply module with a mass of approximately 36 metric tons from Low Earth Orbit to the first Earth-Moon libration point (LL1) within 270 days. Following an examination of propulsion and power technology options, a SEP transfer vehicle design was selected that incorporated large-area (approx. 2700 sq m) thin film solar arrays and a clustered engine configuration of eight 50 kW gridded ion thrusters mounted on an articulated boom. Refinement of the SEP vehicle design was performed iteratively to properly estimate the required xenon propellant load for the out-bound orbit transfer. The SEP vehicle performance, including the xenon propellant estimation, was verified via the SNAP trajectory code. Further efforts are underway to extend this system model to other orbit transfer missions.
英文关键词	SOLAR ELECTRIC PROPULSION ION ENGINES THRUST CHAMBERS ORBIT DECAY DESIGN ANALYSIS CARGO TRAJECTORIES AEROSPACE SYSTEMS LIBRATION LOADS (FORCES) LOW EARTH ORBITS PROPELLANTS TECHNOLOGY TRANSFER THIN FILMS XENON
出版年	2002
报告类型	Technical Report
语种	英语
国家	美国
URL	http://hdl.handle.net/2060/20020085156
资源类型	科技报告
条目标识符	http://119.78.100.177/qdio/handle/2XILL650/259295
推荐引用方式 GB/T 7714	Sarver-Verhey, Timothy R.,Kerslake, Thomas W.,Rawlin, Vincent K.,et al. Solar Electric Propulsion Vehicle Design Study for Cargo Transfer to Earth-moon L1,2002.