Polar Satellite Launch Vehicle

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PS4 has carried hosted payloads like AAM on PSLV-C8, [42] Rubin 9.1/Rubin 9.2 on PSLV-C14 [56] and mRESINS on PSLV-C21. [57] But now, PS4 is being augmented to serve as a long duration orbital platform after completion of primary mission. PS4 Orbital Platform (PS4-OP) will have its own power supply, telemetry package, data storage and attitude control for hosted payloads. [58] [59] [60]

On PSLV-C37 and PSLV-C38 campaigns, [61] as a demonstration PS4 was kept operational and monitored for over ten orbits after delivering spacecraft. [62] [63] [64]

PSLV-C44 was the first campaign where PS4 functioned as independent orbital platform for short duration as there was no on-board power generation capacity. [65] It carried KalamSAT-V2 as a fixed payload, a 1U cubesat by Space Kidz India based on Interorbital Systems kit. [66] [67]

On PSLV-C45 campaign, the fourth stage had its own power generation capability as it was augmented with an array of fixed solar cells around PS4 propellant tank. [68] The three payloads hosted on PS4-OP were the Advanced Retarding Potential Analyzer for Ionospheric Studies (ARIS 101F) by IIST, [69] an experimental AIS payload by ISRO, and AISAT by Satellize. [70] To function as orbital platform, fourth stage was put in spin-stabilized mode using its RCS thrusters. [71]

On the PSLV-C53 campaign, the PS4-OP is referred to as the PSLV Orbital Experimental Module (POEM), and it hosted six payloads. POEM was the first PSLV fourth stage based orbital platform to be actively stabilised using Helium based cold gas thrusters after the primary mission and stage passivization. [72] [73] [74] [75]

Payload fairing

PSLV heat shield at HAL Aerospace Museum, Bengaluru. PSLV heat shield at HAL museum, Bengaluru (Ank Kumar) 01.jpg
PSLV heat shield at HAL Aerospace Museum, Bengaluru.

Payload fairing of PSLV, also referred as its "Heatshield" consists of a conical upper section with spherical nose-cap, a cylindrical middle section and a lower boat-tail section. Weighing 1,182 kilograms (2,606 lb), it has 3.2 meter diameter and 8.3 meter height. [76] It has Isogrid construction and is made out of 7075 aluminum alloy with a 3 mm thick steel nose-cap. [77] [78] The two halves of fairing are separated using a pyrotechnic device based jettisoning system consisting horizontal and lateral separation mechanisms. [79] To protect spacecraft from damage due to excessive acoustic loads during launch, the heatshield interior is lined with acoustic blankets. [28]

Polar Satellite Launch Vehicle
PSLV C-35 at the launch pad (cropped).jpg
PSLV-C35 on the SDSC FLP
Function Medium-lift launch system
ManufacturerISRO
Country of originIndia
Cost per launch 130 crore (equivalent to 153 croreorUS$19 million in 2023)
- 200 crore (equivalent to 235 croreorUS$29 million in 2023) [1]
Size
Height44 m (144 ft)
Diameter2.8 m (9 ft 2 in)
MassPSLV-G: 295,000 kg (650,000 lb)
PSLV-CA: 230,000 kg (510,000 lb)
PSLV-XL: 320,000 kg (710,000 lb) [2]
Stages4
Capacity
Payload to LEO (200 km @ 30° inclination)
Mass
  • G: 3,200 kg (7,100 lb)
  • CA: 2,100 kg (4,600 lb)
  • XL: 3,800 kg (8,400 lb)
[3] [4]
Stage 1Stage 2Stage 3Stage 4
PitchSITVCEngine GimbalNozzle FlexEngine Gimbal
YawSITVCEngine GimbalNozzle FlexEngine Gimbal
RollRCT and SITVC in 2 PSOMsHRCM Hot Gas Reaction Control MotorPS4 RCSPS4 RCS

Variants

ISRO has envisaged a number of variants of PSLV to cater to different mission requirements. There are currently two operational versions of the PSLV — the core-alone (PSLV-CA) without strap-on motors, and the (PSLV-XL) version, with six extended length (XL) strap-on motors carrying 12 tonnes of HTPB based propellant each. [80] These configurations provide wide variations in payload capabilities up to 3,800 kg (8,400 lb) in LEO and 1,800 kg (4,000 lb) in sun-synchronous orbit.

PSLV-G

The standard or "Generic" version of the PSLV, PSLV-G had four stages using solid and liquid propulsion systems alternately and six strap-on motors (PSOM or S9) with 9 tonne propellant loading. It had capability to launch 1,678 kg (3,699 lb) to 622 km (386 mi) into sun-synchronous orbit. PSLV-C35 was the last operational launch of PSLV-G before its discontinuation. [81] [82] [83]

PSLV-CA

The PSLV-CA, CA meaning "Core Alone", model premiered on 23 April 2007. The CA model does not include the six strap-on boosters used by the PSLV standard variant but two SITVC tanks with Roll Control Thruster modules are still attached to the side of the first stage with addition of two cylindrical aerodynamic stabilizers. [49] [83] The fourth stage of the CA variant has 400 kg (880 lb) less propellant when compared to its standard version. [49] It currently has capability to launch 1,100 kg (2,400 lb) to 622 km (386 mi) Sun-synchronous orbit. [84]

PSLV-XL

PSLV-XL is the upgraded version of Polar Satellite Launch Vehicle in its standard configuration boosted by more powerful, stretched strap-on boosters with 12 tonne propellant load. [49] Weighing 320 t (310 long tons; 350 short tons) at lift-off, the vehicle uses larger strap-on motors (PSOM-XL or S12) to achieve higher payload capability. [85] On 29 December 2005, ISRO successfully tested the improved version of strap-on booster for the PSLV. [86] The first use of PSLV-XL was the launch of Chandrayaan-1 by PSLV-C11. The payload capability for this variant is 1,800 kg (4,000 lb) to Sun-synchronous orbit. [84]

PSLV-DL

PSLV-DL variant has only two strap-on boosters with 12 tonne propellant load on them. PSLV-C44 on 24 January 2019 was the first flight to use PSLV-DL variant of Polar Satellite Launch Vehicle. [87] [88] It is capable of launching 1,257 kg (2,771 lb) to 600 km (370 mi) Sun-synchronous orbit. [5]

PSLV-QL

PSLV-C45 lift off PSLV C45 EMISAT campaign 22.jpg
PSLV-C45 lift off

PSLV-QL variant has four ground-lit strap-on boosters, each with 12 tonnes of propellant. PSLV-C45 on 1 April 2019 was the first flight of PSLV-QL. [89] It has the capacity to launch 1,523 kg (3,358 lb) to 600 km (370 mi) Sun-synchronous orbit. [5]

PSLV-3S (concept)

PSLV-3S was conceived as a three-staged version of PSLV with its six strap-on boosters and second liquid stage removed. The total lift-off mass of PSLV-3S was expected to be 175 tonnes with capacity to place 500 kg in 550 km low Earth orbit. [84] [90] [91] [92] [93]

Launch profile

PSLV - XL:

[94] [95] [96]

Launch statistics

As of January 1,2024 the PSLV has made 60 launches, with 57 successfully reaching their planned orbits, two outright failures and one partial failure, yielding a success rate of 95% (or 97% including the partial failure). [97] All launches have occurred from the Satish Dhawan Space Centre, known before 2002 as the Sriharikota Range (SHAR).

Launch system status
  Retired
VariantLaunchesSuccessesFailuresPartial failures
PSLV-G (Standard)121011
PSLV-CA (Core Alone)171700
PSLV-XL (Extended) [2] 252410
PSLV-DL [2] 4400
PSLV-QL [2] 2200
Total as of January 2024 [98] 605721
Decade-wise summary of PSLV launches
DecadeSuccessfulPartial successFailureTotal
1990s3115
2000s110011
2010s330134
2020s100010
Total571260

See also

Related Research Articles

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<span class="mw-page-title-main">Satish Dhawan Space Centre</span> Spaceport in Sriharikota, Andhra Pradesh, India

Satish Dhawan Space Centre – SDSC, is the primary spaceport of the Indian Space Research Organisation (ISRO), located in Sriharikota, Andhra Pradesh.

<span class="mw-page-title-main">Augmented Satellite Launch Vehicle</span> Retired Indian small-lift launch vehicle

The Augmented Satellite Launch Vehicle or Advanced Satellite Launch Vehicle was a small-lift launch vehicle five-stage solid-fuel rocket developed by the Indian Space Research Organisation (ISRO) to place 150 kg satellites into LEO. This project was started by India during the early 1980s to develop technologies needed for a payload to be placed into a geostationary orbit. Its design was based on Satellite Launch Vehicle. ISRO did not have sufficient funds for both the Polar Satellite Launch Vehicle programme and the ASLV programme at the same time and the ASLV programme was terminated after the initial developmental flights. The payloads of ASLV were Stretched Rohini Satellites.

<span class="mw-page-title-main">LVM3</span> Indian expendable medium-lift launch vehicle, developed by ISRO

The Launch Vehicle Mark-3 or LVM3 is a three-stage medium-lift launch vehicle developed by the Indian Space Research Organisation (ISRO). Primarily designed to launch communication satellites into geostationary orbit, it is also due to launch crewed missions under the Indian Human Spaceflight Programme. LVM3 has a higher payload capacity than its predecessor, GSLV.

PSLV-C34 was the 36th mission of the PSLV program and 14th mission of PSLV in XL configuration. The PSLV-C34 successfully carried and deployed 20 satellites in the Sun-synchronous orbit. With a launch mass of 320,000 kilograms (710,000 lb) and payload mass of 1,288 kilograms (2,840 lb), the C34 set a new record of deploying the maximum number of satellites by Indian Space Research Organisation in a single mission. The PSLV-C34 carried One Cartosat-2 satellite, SathyabamaSat, Swayam & 17 other satellites from United States, Canada, Germany & Indonesia.

PSLV-C35 was the successful mission of the Polar Satellite Launch Vehicle program which set eight satellites in space. It was launched on 26 September 2016 by Indian Space Research Organisation (ISRO) from the Satish Dhawan Space Centre at Sriharikota.

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, BIRD and PROBA. 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.

PSLV-C5 was the fifth operational launch and overall eighth mission of the Polar Satellite Launch Vehicle program. This launch was also the fifty-second launch by the Indian Space Research Organisation (IRSO) since its first mission on 1 January 1962. The vehicle carried and injected India's remote sensing satellite Resourcesat-1 into a Sun-synchronous orbit; this was the heaviest and most sophisticated satellite built by IRSO through 2003. PSLV-C5 was launched at 04:52 hours Coordinated Universal Time on 17 October 2003 from Satish Dhawan Space Centre.

<span class="mw-page-title-main">PSLV-C6</span>

PSLV-C6 was the sixth operational launch and overall ninth mission of the PSLV program. This launch was also the fifty-fourth launch by Indian Space Research Organisation since its first mission on 1 January 1962. The vehicle carried and injected India's two satellites; Cartosat-1 and HAMSAT into the Sun-synchronous orbit. PSLV-C6 was launched at 04:44 hours Coordinated Universal Time on 5 May 2005 from the second launch pad of the Satish Dhawan Space Centre.

<span class="mw-page-title-main">IRNSS-1H</span>

IRNSS-1H was the eighth in the Indian Regional Navigational Satellite System (IRNSS) series of satellites, after IRNSS-1A, IRNSS-1B, IRNSS-1C, IRNSS-1D, IRNSS-1E, IRNSS-1F and IRNSS-1G. It was lost in the launch failure of PSLV-C39 on August 31, 2017.

<span class="mw-page-title-main">Small Satellite Launch Vehicle</span> Indian small-lift launch vehicle

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<span class="mw-page-title-main">PSLV-C42</span> 44th mission of the Indian Polar Satellite Launch Vehicle program

PSLV-C42 was the 44th mission of the Indian Polar Satellite Launch Vehicle (PSLV) program and its 12th mission in the Core Alone (CA) configuration. PSLV-C42 successfully carried and deployed 2 Earth observation satellites in Sun-synchronous orbits at an altitude of 588 kilometres (365 mi). It was launched on 16 September 2018 by the Indian Space Research Organisation (ISRO) from the first launch pad of the Satish Dhawan Space Centre at Sriharikota, Andhra Pradesh. The two international satellites were launched as part of a commercial arrangement between Surrey Satellite Technology Limited (SSTL) and ISRO's commercial arm Antrix Corporation Limited, run under the auspices of the Indian Government's Department of Space.

<span class="mw-page-title-main">PSLV-C44</span>

The PSLV-C44 was the 46th mission of the Indian Polar Satellite Launch Vehicle (PSLV) program. It was the first flight of PSLV-DL, having 2 strap-on boosters and placed a primary payload Microsat-R and a secondary payload of Kalamsat V2 in Sun-synchronous orbits.

<span class="mw-page-title-main">PSLV-C45</span>

The PSLV-C45 is the 47th mission of the Indian Polar Satellite Launch Vehicle (PSLV) program. The Polar Satellite Launch Vehicle (PSLV)-C45 was launched on 1 April 2019 with a payload of 29 satellites, including one for electronic intelligence, along with 28 customer satellites from other countries.

<span class="mw-page-title-main">PSLV-C51</span>

The PSLV-C51 is the 53rd mission of the Indian Polar Satellite Launch Vehicle (PSLV) program. The Polar Satellite Launch Vehicle (PSLV)-C51 was launched at 04:54 (UTC) / 10:24 (IST) on 28 February 2021 with the main payload from Brazil, INPE's Amazônia-1 and 18 other ride-sharing small satellites.

<span class="mw-page-title-main">PSLV-C54</span> Indian satellite launch mission

The PSLV-C54 was the 56th mission of the Indian Space Research Organisation's Polar Satellite Launch Vehicle (PSLV). It was launched on 26 November 2022 with the Oceansat-3 satellite and Thybolt nanosatellites of Dhruva Space from Satish Dhawan Space Centre, Sriharikota, Andhra Pradesh, India.

<span class="mw-page-title-main">PSLV-C55</span> Indian satellite launch mission

The PSLV-C55 was the 57th mission of Indian Space Research Organisation's Polar Satellite Launch Vehicle (PSLV) and the 16th flight of the PSLV-CA variant.

The Next Generation Launch Vehicle or NGLV is a three-stage partially reusable rocket, currently under development by the Indian Space Research Organisation (ISRO). This vehicle is designed to replace currently operational systems like PSLV, GSLV and LVM3.

<span class="mw-page-title-main">PSLV C7</span> Polar Satelite Launch Vehicle mission by ISRO

PSLV-C7 was a mission of the Indian Polar Satellite Launch Vehicle (PSLV) rocket, launched on January 10, 2007, by the Indian Space Research Organisation (ISRO) from the Satish Dhawan Space Centre at Sriharikota, Andhra Pradesh.

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