GSLV
GSLV familyIndian Space Research OrganizationActive
GSLVGeosynchronous Satellite Launch Vehicle abbreviated as GSLV, is an expendable launch system operated by the Indian Space Research Organisation (ISRO).
Specifications
- Thrust
- 4,860 kN
- Height
- 49.13 m
- Diameter
- 2.8 m
- Launch mass
- 414 t
- Stages
- 3
- Launch cost
- $47M
- LEO capacity
- 5,000 kg
- GTO capacity
- 2,500 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
6flightswith a definitive outcome
33.3%success rate2 of 6
4failuresincluding partial failures
0success streakcurrent
First flight April 18, 2001 · latest December 25, 2010
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for GSLV flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 2001 | 0 | 1 | 1 |
| 2002 | 0 | 0 | 0 |
| 2003 | 1 | 0 | 1 |
| 2004 | 1 | 0 | 1 |
| 2005 | 0 | 0 | 0 |
| 2006 | 0 | 1 | 1 |
| 2007 | 0 | 1 | 1 |
| 2008 | 0 | 0 | 0 |
| 2009 | 0 | 0 | 0 |
| 2010 | 0 | 1 | 1 |