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Chang'e 5-T1 () is an experimental unmanned lunar mission that was launched on 23 October 2014 by the China National Space Administration (CNSA) to conduct atmospheric re-entry tests on the capsule design planned to be used in the Chang'e 5 mission.〔〔(【引用サイトリンク】 title=CLunar mission：craft to conduct re-entry tests before 2015 )〕〔(【引用サイトリンク】 title=China's Lunar Probe Tester Ready for Chang'e 5 Mission )〕 As the final part of the Chinese Lunar Exploration Program, Chang'e 5, scheduled for 2017, will be a Moon sample return mission. Like its predecessors, the spacecraft is named after the Chinese Moon goddess Chang'e. * Xiaofei, the return capsule of Chang'e 5-T1, landed in Siziwang Banner, Inner Mongolia on 31 October 2014, 22:42 UTC. * CE-5-T1 Service Module entered lunar orbit〔http://news.xinhuanet.com/english/china/2015-01/13/c_133915882.htm〕 by January 13, 2015 - initial orbit is 200 x 5300 km with period of 8 hours. ==Characteristics== It consisted of a DFH-3A "Chang'e 2 type" spacecraft featuring the Chang'e 5 return capsule, launched by a Long March 3C rocket into a lunar free return trajectory. It looped behind the Moon and returned to Earth, with the return capsule testing the high speed atmospheric skip reentry. The DFH-3A "service module" remained in orbit around the Earth before being relocated via Earth-Moon L2 to lunar orbit by 13 January 2015, where it will use its remaining 800 kg of fuel to test maneuvers key to future lunar missions.〔(【引用サイトリンク】url=http://www.spaceflight101.com/change-5-test-mission-updates.html )〕 In February and March the DFH-3A "service module" will perform 2 "virtual target" rendezvous tests for the future CE-5 mission. In April 2015 the small monitoring camera will be used to obtain higher resolution photos of CE-5's landing zone. 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Chang'e 5-T1」の詳細全文を読む スポンサード リンク
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