Temir Kazyk

Rockets / PSLV

PSLV

EXPENDABLE 4-STAGE LAUNCH VEHICLE

ACTIVE
PSLV

Technical Overview

Length height
44 m
Diameter radio_button_unchecked
2.8 m
Launch Mass scale
295 t
Payload to LEO rocket
3,800 kg
Payload to GTO public
1,200 kg
Payload to SSO satellite_alt
1,750 kg

Engine Details

PSLV

PSLV

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).

Reusability

Expendable

Stages

4

Liftoff Thrust

4,847 kN

Launch Cost

$21,000,000

Maiden Flight

1993-09-20

Fastest Turnaround

P325DT5H30M40S

Flight History

*Since 1993-09-20
rocket_launch

Total Launches

12

trending_up 8 consecutive successes
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Successful Launches

10

verified 83% success rate
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Failed Launches

2

schedule 2 pending