Ivar asteroid rendezvous mission system scenario and trajectory design
The asteroid exploration opportunities are searched and calculated with launch dates in 2006 to2010, and with asteroid Ivar 1627 as the target, the spacecraft and its subsystems are designed and analyzed,and the transfer trajectory is designed using △VEGA technology for the asteroid rendezvous. The design resultssatisfied the energy requirements for small explorers.
作 者： 崔平远 李立涛 崔祜涛 栾恩杰 吴伟仁 田玉龙 作者单位： 崔平远,李立涛,崔祜涛(Deep Space Exploration Research Center, Harbin Institute of Technology, Harbin 150001, China)栾恩杰,吴伟仁,田玉龙(China National Space Administration, Beijing 100037, China)
刊 名： 哈尔滨工业大学学报(英文版) EI 英文刊名： JOURNAL OF HARBIN INSTITUTE OF TECHNOLOGY(NEW SERIES) 年，卷(期)： 2003 10(3) 分类号： V412.4 关键词： trajectory design rendezvous spacecraft system design asteroid exploration