GSLV·Indian Space Research Organization
GSLV
active
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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