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： 崔平遠(yuǎn) 李立濤 崔祜濤 欒恩杰 吳偉仁 田玉龍 作者單位： 崔平遠(yuǎn),李立濤,崔祜濤(Deep Space Exploration Research Center, Harbin Institute of Technology, Harbin 150001, China)欒恩杰,吳偉仁,田玉龍(China National Space Administration, Beijing 100037, China)
刊 名： 哈爾濱工業(yè)大學(xué)學(xué)報(bào)(英文版) EI 英文刊名： JOURNAL OF HARBIN INSTITUTE OF TECHNOLOGY(NEW SERIES) 年，卷(期)： 2003 10(3) 分類號(hào)： V412.4 關(guān)鍵詞： trajectory design rendezvous spacecraft system design asteroid exploration