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GSLV  
Initial Operational Capability (IOC): 20 January 2017
Maiden Flight: 18 December 2014
Total Production: ?
Unitary Cost: USD$40 million
Also Known As: Geosynchronous Satellite Launch Vehicle and GSLV Mark III
Origin: India
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.

GSLV Specifications

Dimensions
Height: 50 meter (1,969 inch)
Weight
Max Lift-off Weight: 416 ton (917,108 pound)
Payload: 11,000 pound (4.99 ton)
Payload to GEO: 2.20 ton (4,850 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)
Shaft-Horse-Power (shp)

GSLV News

There is 1 news
on 18 Dec 2014
Thursday, December 18, 2014India Successfully Conducts First Test Launch of GSLV Mark 3 Rocket

Operators & Related Equipment


OperatorsItems

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