Kalpana Kalpana (Editor)

PSLV C3

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Website
  
ISRO website

Mass
  
1,294 kg

Apogee
  
586,700 m

Manufacturer
  
ISRO

Mission duration
  
28 minutes

Launch mass
  
294,000 kg

PSLV-C3

Mission type
  
Deployment of three satellites.

Spacecraft
  
Polar Satellite Launch Vehicle

Spacecraft type
  
Expendable launch vehicle

Payload mass
  
1,294 kilograms (2,853 lb)

Rocket
  
Polar Satellite Launch Vehicle

Operator
  
Indian Space Research Organisation

Launch site
  
Satish Dhawan Space Centre

Isro pslv c37 launch with onboard camera and stage satellite separation events


PSLV-C3 was the third operational launch and overall sixth mission of the PSLV program. This launch was also the forty-sixth launch by Indian Space Research Organisation since its first mission on 1 January 1962. The vehicle carried three satellites which were deployed in the Sun-synchronous Low Earth orbit. The vehicle carried Technology Experiment Satellite (Indian experimental earth observation satellite), BIRD (German earth observation satellite) and PROBA (experimental satellite from Belgium). This was India's and ISRO's second commercial spaceflight. PSLV-C3 was launched at 10:23 a.m. IST on 22 October 2001 from Satish Dhawan Space Centre (then called "Sriharikota Launching Range").

Contents

Mission highlights

  • Third operational launch of the PSLV program.
  • Overall sixth mission of the PSLV program.
  • Second commercial launch by ISRO.
  • Three satellites injected in Sun-synchronous low Earth orbit.
  • Mission parameters

  • Mass:
  • Total liftoff weight: 294,000 kilograms (648,000 lb)
  • Payload weight: 1,294 kilograms (2,853 lb)
  • Overall height: 44.4 metres (145.7 ft)
  • Propellant:
  • First stage: Solid HTPB based (138.0 + 54 tonnes)
  • Second stage: Liquid UDMH + N2O4 (40 tonnes)
  • Third stage: Solid HTPB based (7 tonnes)
  • Fourth stage: Liquid MMH + MON (2.0 tonnes)
  • Engine:
  • First stage: S139
  • Second stage: Vikas
  • Third stage:
  • Fourth stage: 2 x PS-4
  • Thrust:
  • First stage: 4,430 + 677 x 6 kN
  • Second stage: 724 kN
  • Third stage: 324 kN
  • Fourth stage: 7.4 x 2 kN
  • Altitude: 586.7 kilometres (365 mi)
  • Maximum velocity:7,593 metres per second (24,911 ft/s) (recorded at time of fourth stage ignition)
  • Duration: 1,658 seconds
  • Payload

    PSLV-C3 carried and deployed total three satellites. Technology Experiment Satellite (TES) was the main payload and BIRD and PROBA were two auxiliary payloads that were mounted on PSLV-C3. In the flight sequence, TES was injected first, followed by BIRD and then PROBA.

    Launch & planned flight profile

    PSLV-C3 was launched at 10:23 a.m. IST on 22 October 2001 from Satish Dhawan Space Centre (then called "Sriharikota Launching Range"). The mission was planned with pre-flight prediction of covering overall distance of 586.668 kilometres (365 mi). Following was the planned flight profile.

    References

    PSLV-C3 Wikipedia