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GSLV Mk-2
ISRO
The Geosynchronous Satellite Launch Vehicle Mark II is an Indian orbital launch vehicle designed to place satellites into geostationary orbit.
First Flight
April 18, 2001
Total Launches
18
Success Rate
75%
Stages
3
Technical Specifications
Dimensions
Height
49 m / 161 ft
Diameter
2.8 m / 9.2 ft
Mass
Total Mass
414,750 kg
914,400 lb
Payload Capacity
LEO
5,000 kg
11,000 lb
GTO
2,500 kg
5,500 lb
Thrust
Liftoff Thrust
4,800 kN
1,079,000 lbf