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Geosynchronous Satellite Launch Vehicle Mk III
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Geosynchronous Satellite Launch Vehicle Mk III : ウィキペディア英語版
Geosynchronous Satellite Launch Vehicle Mk III



|family =

|status = Development
|sites = Satish Dhawan Space Centre SLP, Andhra Pradesh, India
|launches = 1 (2 stage version)
|success = 1 (2 stage version)
|fail =
|partial =
|first = 18 December 2014 (2 stage version; sub-orbital flight)
|last =
|payloads =

|stagedata =






}}
The GSLV-III or Geosynchronous Satellite Launch Vehicle Mark III ((ヒンディー語:भूस्थिर उपग्रह प्रक्षेपण यान एमके-३); also called LVM3)〔 is a launch vehicle developed by the Indian Space Research Organisation (ISRO).
It is intended to launch satellites into geostationary orbit and as a launcher for an Indian crew vehicle. The GSLV-III features an Indian cryogenic third stage and a higher payload capacity than the current GSLV.〔(GSLV MkIII, the next milestone : Interview: K. Radhakrishnan ) Frontline 7 February 2014〕
==History==
Development for the GSLV-III began in the early 2000s, with the first launch planned for 2009-2010.〔
〕 Several factors have delayed the program, including the 15 April 2010 failure of the ISRO-developed cryogenic upper stage on the GSLV Mk II.〔
A suborbital flight test of the GSLV-III launcher, with a passive cryogenic third stage, was successfully carried out on 18 December 2014, and was used to test a crew module on a suborbital trajectory. The first orbital flight is planned to take place in 2017.〔(【引用サイトリンク】title=Now, ISRO Well on Course to Test Giant Rocket GSLV Mk-III )〕 The first flight with a crew on board would take place after 2020.〔

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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