Geosynchronous Satellite Launch Vehicle

Last updated

As of February 17,2024, rockets from the GSLV family have made 16 launches, resulting in 10 successes, four failures, and two partial failures. [32] All launches have occurred from the Satish Dhawan Space Centre, known before 2002 as the Sriharikota Range (SHAR).

Launch system status
  Active
  Retired
GSLV
GSLV logo.svg
GSLV-F14, INSAT-3DS - Launch Vehicle at Second Launch Pad (SLP).webp
GSLV-F14 carrying INSAT-3DS at the Satish Dhawan Space Centre Second Launch Pad
Function Medium-lift Launch System
ManufacturerISRO
Country of originIndia
Cost per launchUS$47 million [1]
Size
Height49.13 m (161.2 ft) [2]
Diameter2.8 m (9 ft 2 in)
Mass414,750 kg (914,370 lb)
Stages3
Capacity
Payload to LEO
Mass6,000 kg (13,000 lb) [3]
Launch sites Satish Dhawan Space Centre
Total launches 16
Success(es)10
Failure(s)4
Partial failure(s)2
First flight
  • Mk.I: 18 April 2001
  • Mk.II: 15 April 2010
Last flight
  • Mk.I: 25 December 2010
  • Mk.II: 17 February 2024
Type of passengers/cargo South Asia Satellite, NavIC
Boosters
No. boosters4 L40 Hs
Height19.7 m (65 ft) [5]
Diameter2.1 m (6 ft 11 in)
Propellant mass42,700 kg (94,100 lb) each
Powered by1 L40H Vikas 2
Maximum thrust760 kN (170,000 lbf) [6]
Total thrust3,040 kN (680,000 lbf)
Specific impulse 262 s (2.57 km/s)
Burn time154 seconds
Propellant N2O4 / UDMH
VariantLaunchesSuccessesFailuresPartial failures
GSLV Mk. I6222
GSLV Mk. II10820
Total as of February 2024 [33] 161042
Decade-wise summary of GSLV Launches
DecadeSuccessfulPartial successFailureTotal
2000s2215
2010s6028
2020s2013
Total102416

See also

Related Research Articles

<span class="mw-page-title-main">Polar Satellite Launch Vehicle</span> Indian expendable launch vehicle for launching satellites, developed by ISRO

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).

<span class="mw-page-title-main">Indian National Satellite System</span> Series of multipurpose geo-stationary satellites launched by ISRO

The Indian National Satellite System or INSAT, is a series of multipurpose geostationary satellites launched by ISRO to satisfy telecommunications, broadcasting, meteorology, and search and rescue operations. Commissioned in 1983, INSAT is the largest domestic communication system in the Indo-Pacific Region. It is a joint venture of the Department of Space, Department of Telecommunications, India Meteorological Department, All India Radio and Doordarshan. The overall coordination and management of INSAT system rests with the Secretary-level INSAT Coordination Committee.

GSAT-3, also known as EDUSAT, was a communications satellite which was launched on 20 September 2004 by the Indian Space Research Organisation. EDUSAT is the first Indian satellite built exclusively to serve the educational sector. It is mainly intended to meet the demand for an interactive satellite-based distance education system for the country.

GSAT-1 was an experimental communications satellite launched aboard the maiden flight of the GSLV rocket. The spacecraft was equipped with instrumentation to test Pulse-code modulation (PCM) transmitting on S-band frequencies and transponders operating in the C-band. The spacecraft was unable to complete its mission after a launch failure left it in a lower than planned orbit and propulsion issues prevented the satellite from correcting this via its own maneuvering system.

<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.

The Tel Aviv University Ultraviolet Explorer, or TAUVEX, is a space telescope array conceived by Noah Brosch of Tel Aviv University and designed and constructed in Israel for Tel Aviv University by El-Op, Electro-Optical Industries, Ltd. acting as Prime Contractor, for the exploration of the ultraviolet (UV) sky. TAUVEX was selected in 1988 by the Israel Space Agency (ISA) as its first priority scientific payload. Although originally slated to fly on a national Israeli satellite of the Ofeq series, TAUVEX was shifted in 1991 to fly as part of a Spektr-RG international observatory, a collaboration of many countries with the Soviet Union leading.

<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.

<span class="mw-page-title-main">GSAT-4</span>

GSAT-4, also known as HealthSat, was an experimental communication and navigation satellite launched in April 2010 by the Indian Space Research Organisation on the maiden flight of the Geosynchronous Satellite Launch Vehicle Mk.II rocket. It failed to reach orbit after the rocket's third stage malfunctioned. The third stage was the first Indian-built cryogenic-fuelled upper stage, and was making its first flight. The ISRO suspects that the failure was caused by the third stage not igniting.

<span class="mw-page-title-main">Vikas (rocket engine)</span> Indian rocket engine

The Vikas is a family of hypergolic liquid fuelled rocket engines conceptualized and designed by the Liquid Propulsion Systems Centre in the 1970s. The design was based on the licensed version of the Viking engine with the chemical pressurisation system. The early production Vikas engines used some imported French components which were later replaced by domestically produced equivalents. It is used in the Polar Satellite Launch Vehicle (PSLV), Geosynchronous Satellite Launch Vehicle (GSLV) and LVM3 for space launch use.

<span class="mw-page-title-main">CE-7.5</span> Cryogenic rocket engine developed by the Indian Space Research Organisation

The CE-7.5 is a cryogenic rocket engine developed by the Indian Space Research Organisation to power the upper stage of its GSLV Mk-2 launch vehicle. The engine was developed as a part of the Cryogenic Upper Stage Project (CUSP). It replaced the KVD-1 (RD-56) Russian cryogenic engine that powered the upper stage of GSLV Mk-1.

GSAT-5P, or GSAT-5 Prime, was an Indian communications satellite which was lost in a launch failure in December 2010. Part of the Indian National Satellite System, it was intended to operate in geosynchronous orbit as a replacement for INSAT-3E.

GSAT-14 is an Indian communications satellite launched in January 2014. It replaced the GSAT-3 satellite, which was launched in 2004. GSAT-14 was launched by a Geosynchronous Satellite Launch Vehicle Mk.II, which incorporated an Indian-built cryogenic engine on the third stage.

KVD-1 was an upper stage LOX/LH2 cryogenic engine developed by the Isayev Design Bureau (now KB KhIMMASH) of Russia in the early 1960s. It is a modified version of the RD-56, developed for a never-completed cryogenic upper stage of the N-1 super-heavy lift rocket, with the goal of enabling crewed lunar missions by the USSR. The KVD-1 produces a thrust of 7.5 tonnes.

<span class="mw-page-title-main">GSAT-19</span>

GSAT-19 is an Indian communications satellite launched by the Indian Space Research Organisation aboard a GSLV Mark III on 5 June 2017.

<span class="mw-page-title-main">GSAT-6A</span> Indian telecommunications satellite

GSAT-6A was a communication satellite launched by the Indian Space Research Organisation (ISRO) It featured a 6-metre (20 ft) unfurlable S-band antenna similar to the one used on GSAT-6. Around 17 minutes after lift-off, the three stage GSLV Mk.II rocket flying on GSLV F08 mission successfully injected the satellite into a geosynchronous transfer orbit. Due to power failure during its orbit raising burns the communication was lost with GSAT-6A before it could reach its final circular geostationary orbit (GSO).

<span class="mw-page-title-main">GSAT-29</span> Indian communication satellite

GSAT-29 is a high-throughput communication satellite developed by the Indian Space Research Organisation (ISRO). The mission aims at providing high-speed bandwidth to Village Resource Centres (VRC) in rural areas. The two Ku and Ka operational payloads will provide communication services to Jammu and Kashmir and Northeast India under Digital India programme. At the time of launch GSAT-29 was the heaviest satellite, weighing 3,423 kg (7,546 lb), that was placed in orbit by an Indian launch vehicle. Approved cost of GSAT-29 is 175.63 crore (US$22 million).

The S139 is a Solid Rocket Booster manufactured by the Indian Space Research Organization at the Satish Dhawan Space Center in the SPROB facility. The rocket motor was first developed for use in the Polar Satellite Launch Vehicle. Later it was utilized in the GSLV MKII. It uses hydroxyl-terminated polybutadiene (HTPB) as a propellant. It has a maximum thrust of 4800 kN.

<span class="mw-page-title-main">GSLV-F12</span> 2023 Indian satellite launch mission

The GSLV F12 is the 15th flight of the GSLV and the 9th flight of Mk2 variant using indigenous Cryogenic engine.

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.

References

  1. "GAO".
  2. 1 2 "Geosynchronous Satellite Launch Vehicle". Archived from the original on 21 October 2015. Retrieved 21 December 2014.
  3. 1 2 "HSFC Presentation from International Space Conference and Exhibition 2021" (PDF). Archived from the original (PDF) on 13 September 2021. Retrieved 7 October 2022.
  4. "ISRO developing vehicle to launch small satellites" . Retrieved 29 August 2018.
  5. 1 2 3 4 5 "GSLV F09 Brochure". ISRO.
  6. 1 2 3 4 "GSLV F08 Brochure". ISRO.
  7. 1 2 "GSLV F11 Brochure". ISRO.
  8. "GSLV Launched Successfully" (PDF). Current Science. 80 (10): 1256. May 2001. Retrieved 12 December 2013.
  9. 1 2 Subramanian, T. S. (17–31 March 2001). "The GSLV Quest". Frontline. Retrieved 12 December 2013.
  10. "GSLV Rocket, Billed 'Naughty Boy'". NDTV. Archived from the original on 11 February 2018. Retrieved 11 February 2018.
  11. Jacob Aron. "India's hefty "naughty boy" rocket comes in from cold". New Scientist. Archived from the original on 11 February 2018. Retrieved 11 February 2018.
  12. Raj, N Gopal (21 April 2011). "The long road to cryogenic technology". The Hindu. Chennai, India. Retrieved 12 December 2013.
  13. Subramanian, T. S. (28 April – 11 May 2001). "The cryogenic quest". Frontline. Retrieved 13 December 2013.
  14. "Why ISRO's New Engine and Mk III Rocket Are Reasons to Forget 1990 Cryogenic Scandal". The Wire. Retrieved 10 February 2018.
  15. "GSLV-F04". ISRO. Archived from the original on 4 January 2014. Retrieved 15 December 2013.
  16. 1 2 "GSLV-D2". ISRO. Archived from the original on 9 August 2013. Retrieved 15 December 2013.
  17. 1 2 "GSLV Launcher". ISRO. Retrieved 17 March 2021.
  18. "Evolution of Indian launch vehicle technologies" (PDF). Current Science. Retrieved 27 January 2014.
  19. "GSLV-D5". Archived from the original on 6 October 2014. Retrieved 4 January 2014.
  20. "ISRO's Cryogenic Stage Fails in Maiden Flight". SpaceNews. Archived from the original on 26 May 2012. Retrieved 27 November 2013.
  21. "GSLV, PSLV flights put off". The Hindu. Chennai, India. 1 January 2010. Archived from the original on 5 January 2010.
  22. "GSLV-F14/INSAT-3DS Gallery". www.isro.gov.in. Retrieved 8 February 2024.
  23. "Space India, April-June 2003" (PDF). July 2003. p. 11. Archived (PDF) from the original on 16 August 2021. Retrieved 16 August 2021.
  24. "GSLV-D3/GSAT-4 Brochure" (PDF). ISRO. Archived from the original (PDF) on 7 February 2014. Retrieved 15 January 2014.
  25. R. V. Perumal; B. N. Suresh; D. Narayana Moorthi; G. Madhavan Nair (25 July 2001). "First developmental flight of geosynchronous satellite launch vehicle (GSLV-D1)" (PDF). Current Science. 81 (2): 167–174. Archived from the original (PDF) on 5 March 2016.
  26. R. V. Perumal; D. Narayana Moorthi; N. Vedachalam; G. Madhavan Nair (10 September 2003). "Second developmental flight of Geosynchronous Satellite Launch Vehicle" (PDF). Current Science. 85 (5): 597–601. Archived from the original (PDF) on 16 February 2018.
  27. "GSLV-F06". ISRO. Archived from the original on 10 August 2013. Retrieved 9 January 2014.
  28. "GSLV-F06 / GSAT-5P mission brochure" (PDF). Archived (PDF) from the original on 9 September 2013.
  29. Clark, Stephen (12 October 2010). "India may seek international help on cryogenic engine". Spaceflight Now. Retrieved 15 July 2011. Besides the new upper stage, the GSLV Mk.2 launched in April was nearly identical to previous versions of the booster
  30. Clark, Stephen (29 March 2018). "India tests upgraded engine tech in successful communications satellite launch". Spaceflight Now. Retrieved 30 March 2018.
  31. "GSLV-F10/EOS-03 Brochure". ISRO. Retrieved 14 August 2021.
  32. "List of GSLV launches". isro.org. ISRO. Archived from the original on 13 August 2021. Retrieved 14 December 2020.
  33. "ISRO GSLV NVS-1 Navic launch highlights | India launches next-gen navigational satellite". India Today. Retrieved 29 May 2023.