There is 1 images added on 5 November 2013
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: ?
There are no reviews so far
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.
Height: 50 meter (1,969 inch)
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)
There is 1 news
on 18 Dec 2014
Operators & Related Equipment
Grand Total ?1
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