Rockets

GSLV·Indian Space Research Organization

GSLV

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Specifications

Status
active
Height
49.13 m
Diameter
2.8 m
Mass
414,000 kg
Stages
3
Thrust
4,860 kN
Payload to LEO
5,000 kg
Payload to GTO
2,500 kg
First flight
2001-04-18
Total launches
6
Success / Fail
2 / 4

GSLVGeosynchronous Satellite Launch Vehicle abbreviated as GSLV, is an expendable launch system operated by the Indian Space Research Organisation (ISRO).

Propulsion

First stage

Vikas725 kN
UDMH / N2O4 · gas-generator
ISROIsp 293s (vac)since 1992

Third stage

CE-7.573 kN
LH2 / LOX · staged-combustion
ISROIsp 454s (vac)since 2010

Payloads it launched

4 loaded