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Initial Operational Capability (IOC):
20 January 2017
18 December 2014
Also Known As: Geosynchronous Satellite Launch Vehicle and GSLV Mark III
Parent System: GSLV
Initial Operational Capability (IOC): 20 January 2017
Maiden Flight: 18 December 2014
Total Production: ?
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Description: The Geosynchronous Satellite Launch Vehicle (GSLV) is an indigenous space launch rocket designed by the Indian Space Research Organisation (ISRO). The GSLV program is aimed at placing payloads into geosynchronous orbits. The rocket propulsion system is based upon cryogenic engine technology developed in India. On April 15, 2010, the ISRO failed to launch the GSLV D3 vehicle due to engine trouble. The rocket fell into the Bay of Bengal 304 seconds after lift-off carrying the 2.2-ton G-Sat communications satellite. The launch on December 25, 2010, also failed soon after lift-off. India successfully launched its first GSLV Mark III rocket on December 18, 2014.
Number of Stages: 3
Height: 43 meter (1,710 inch)
Max Lift-off Weight: 640 ton (1,410,935 pound)
Payload: 11,000 pound (4.99 ton)
Payload to GEO: 2,200 kilogram (4,850 pound)
Payload to GTO: 4,000 kilogram (8,818 pound)
Payload to LEO: 10,000 kilogram (22,046 pound)
CEP: Circular Error Probable
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
There are 2 news between
18 Dec 2014 and 5 Jun 2017
Operators & Related Equipment
Grand Total ?1
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