GSLV Mk. II (Indian Space Research Organization)
The GSLV Mk. II is a non-reusable, active launch vehicle manufactured by Indian Space Research Organization (established in 1969). It undertook its inaugural launch on 04/15/2010.
Geosynchronous Satellite Launch Vehicle Mark II (GSLV Mk II) is the largest launch vehicle developed by India, which is currently in operation. 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.
GSLV Mk. II Specifications
| Length | 49 m |
|---|---|
| Diameter | 2.8 m |
| Stages | 3 |
| Launch Mass | 401 T |
| Takeoff Thrust | 7420 kN |
| Apogee | 40000 km |
| GTO Capacity | 2500 kg |
GSLV Mk. II Launch Record
| Total Launches | 13 |
|---|---|
| Successful Launches | 11 |
| Failed Launches | 2 |
| Pending Launches | 5 |
| Consecutive Successful Launches | 5 |
Manufacturer
Chairman: V. Narayanan
The Indian Space Research Organisation (ISRO) is the space agency of the Government of India headquartered in the city of Bangalore. Its vision is to "harness space technology for national development while pursuing space science research and planetary exploration."