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PSLV·Indian Space Research Organization

PSLV

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Specifications

Status
active
Height
44 m
Diameter
2.8 m
Mass
295,000 kg
Stages
4
Thrust
4,847 kN
Payload to LEO
3,800 kg
Payload to GTO
1,200 kg
First flight
1993-09-20
Total launches
12
Success / Fail
10 / 2

The Polar Satellite Launch Vehicle (PSLV) is an expendable medium-lift launch vehicle designed and operated by the Indian Space Research Organisation (ISRO). It was developed to allow India to launch its Indian Remote Sensing (IRS) satellites into sun-synchronous orbits, a service that was, until the advent of the PSLV in 1993, commercially available only from Russia. PSLV can also launch small size satellites into Geostationary Transfer Orbit (GTO).

Propulsion

Second stage

Vikas725 kN
UDMH / N2O4 · gas-generator
ISROIsp 293s (vac)since 1992PS2

Payloads it launched

28 loaded
PRATHAM
LEO
ALSAT-2B
LEO
ALSAT-1B
LEO
ALSAT-1N
LEO
PISAT
LEO
SCATSAT 1
LEO
PATHFINDER 1
LEO
CANX-7
LEO
YOUTHSAT
LEO
RESOURCESAT-2
LEO
X-SAT
LEO
CARTOSAT-2 (IRS-P7)
LEO
LAPAN-TUBSAT
LEO
SRE-1
LEO
PEHUENSAT 1 (PO-63)
LEO
IRS-P5 (CARTOSAT-1)
LEO
HAMSAT (VO-52)
LEO
IRS-P6 (RESOURCESAT-1)
LEO
KALPANA-1 (METSAT 1)
GEO
BIRD 2
LEO
PROBA-1
LEO
TES
LEO
IRS-P4 (OCEANSAT-1)
LEO
KITSAT 3
LEO
DLR-TUBSAT
LEO
IRS-1D
LEO
IRS-P3
LEO
IRS-P2
LEO