Katana VentraIP

Polar Satellite Launch Vehicle

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, only commercially available from Russia. PSLV can also launch small size satellites into Geostationary Transfer Orbit (GTO).[11]

Function

ISRO

India

130 crore (equivalent to 153 crore or US$18 million in 2023)
-200 crore (equivalent to 235 crore or US$28 million in 2023)[1]

44 m (144 ft)

2.8 m (9 ft 2 in)

PSLV-G: 295,000 kg (650,000 lb)
PSLV-CA: 230,000 kg (510,000 lb)
PSLV-XL: 320,000 kg (710,000 lb)[2]

4

  • G: 3,200 kg (7,100 lb)
  • CA: 2,100 kg (4,600 lb)
  • XL: 3,800 kg (8,400 lb)
[3][4]

  • G: 1,600 kg (3,500 lb)
  • CA: 1,100 kg (2,400 lb)
  • XL: 1,750 kg (3,860 lb)
[3][2][5]

1,425 kg (3,142 lb)
(PSLV-XL)[2][5]

  • G: 1,150 kg (2,540 lb)
  • XL: 1,300 kg (2,900 lb)
[3][6]

Active

60

57

2

1

  • PSLV-G: 20 September 1993
  • PSLV-CA: 23 April 2007
  • PSLV-XL: 22 October 2008
  • PSLV-DL: 24 January 2019
  • PSLV-QL: 1 April 2019

  • PSLV-G: 26 September 2016
  • PSLV-CA: 30 July 2023
  • PSLV-XL: 2 September 2023
  • PSLV-DL: 1 January 2024
  • PSLV-QL: 11 December 2019

6

510 kN (110,000 lbf)

262 s (2.57 km/s)

44 s

6 (XL)
4 (QL)
2 (DL)

12 m (39 ft)[7]

1 m (3 ft 3 in)

12,200 kg (26,900 lb) each

off

703.5 kN (158,200 lbf)[8]

4,221 kN (949,000 lbf) (XL)
2,814 kN (633,000 lbf) (QL)
1,407 kN (316,000 lbf) (DL)

262 s (2.57 km/s)

70 s

20 m (66 ft)[7]

2.8 m (9 ft 2 in)

138,200 kg (304,700 lb) each[7][2]

4,846.9 kN (1,089,600 lbf)[8]

237 s (2.32 km/s) (sea level)
269 s (2.64 km/s) (vacuum)

110 s

12.8 m (42 ft)[7]

2.8 m (9 ft 2 in)

42,000 kg (93,000 lb) each[7]

1 Vikas

803.7 kN (180,700 lbf)[8]

293 s (2.87 km/s)

133 s

3.6 m (12 ft)[7]

2 m (6 ft 7 in)

7,600 kg (16,800 lb) each[7]

S-7[9]

250 kN (56,000 lbf)

295 s (2.89 km/s)

113.5 s[10]

3 m (9.8 ft)[7]

1.3 m (4 ft 3 in)

2,500 kg (5,500 lb) each[7]

2 x L-2-5[9]

14.66 kN (3,300 lbf)[8]

308 s (3.02 km/s)

525 s

Some notable payloads launched by PSLV include India's first lunar probe Chandrayaan-1, India's first interplanetary mission, Mars Orbiter Mission (Mangalyaan), India's first space observatory, Astrosat and India's first Solar mission, Aditya-L1.[2]


PSLV has gained credibility as a leading provider of rideshare services for small satellites, owing to its numerous multi-satellite deployment campaigns with auxiliary payloads, usually ride-sharing along with an Indian primary payload.[12] As of June 2022, PSLV has launched 345 foreign satellites from 36 countries.[13] Most notable among these was the launch of PSLV-C37 on 15 February 2017, successfully deploying 104 satellites in Sun-synchronous orbit, tripling the previous record held by Russia for the highest number of satellites sent to space on a single launch,[14][15] until 24 January 2021, when SpaceX launched the Transporter-1 mission on a Falcon 9 rocket carrying 143 satellites into orbit.[16]


Payloads can be integrated in tandem configuration employing a Dual Launch Adapter.[17][18] Smaller payloads are also placed on equipment deck and customized payload adapters.[19]

The PS1 ignites at T+0 providing 4846  kN of thrust.

Within T+1, 4 out of the 6 boosters ignite on ground, each producing 703 kN of thrust. 7658 kN of total thrust is produced by the combined propulsion of the PSOMs and the PS1.

At around T+23/26, the remaining 2 unlit boosters are air-lit bringing the rocket at its maximum thrust capacity.

At T+1:10, the first 4 ground-lit PSOMs have depleted its propellant and now separates and falls down to the ocean. The remaining 2 PSOMs and the PS1 continue to burn.

At T+1:35, the remaining 2 PSOMs complete its 70 seconds burn and separate, leaving the rocket in a Core- Alone configuration.

At T+1:50, the PS1 has completed its 110-second burn and it separates and the inside the PS2 ignites.

Vikas Engine

The second stage burns for around 130 seconds and around T+4 minutes, the second stages shuts off and separates.

The third stage, which is a solid rocket booster, and burns 80 seconds and then coasts for the remainder of time and around T+8/10 minutes, it separates and the 4th stage ignites to give the rocket a final push into the orbit.

This 4th stage burn is highly variable and depends on the mass and number of payloads and usually is around 500 seconds long. The 4th stage may shut off around T+16/18 minutes followed by the Payload Deployment.

PSLV - XL:


[97][98][99]

Geosynchronous Satellite Launch Vehicle

LVM3

Next Generation Launch Vehicle

Comparison of orbital launchers families

2,000 to 20,000 kg to LEO

Medium-lift launch vehicle

Comparison of orbital rocket engines

Comparison of orbital launch systems

Archived 22 December 2016 at the Wayback Machine

PSLV : Official ISRO Page

India in Space PSLV page