Geosynchronous Satellite Launch Vehicle Mark II (GSLV Mk II) is a launch vehicle developed by India and is currently in operation for launching 2t class communication satellites. This fourth generation launch vehicle is a three stage vehicle with four liquid strap-ons. The indigenously developed cryogenic Upper Stage (CUS), which is flight proven, forms the third stage of GSLV Mk II. From January 2014, the vehicle has achieved four consecutive successes.
Vehicle Specifications
Height:
49.13 m
Diameter:
3.4m
Number of Stages:
3
Lift Off Mass:
414.75t
First Flight:
April 18, 2001
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