LVM3

GSLV - Mk III
	File:GSLV Mk III mockup.jpg Mockup of Geosynchronous Satellite Launch Vehicle III
Function	Mid-Heavy Lift Launch System
Manufacturer	ISRO
Country of origin	India
Size
Height	42.4 m
Diameter	4.0 m
Mass	630,000 Kg
Stages	2
Capacity
Payload to LEO	10,000 kg
Payload to; GTO	4,000–5000 kg
Launch history
Status	In Development
Launch sites	Satish Dhawan Space Centre
First flight	Scheduled for 2014
Boosters - S-200
No. boosters	2
Engines	1 Solid
Thrust	5151 kn
Burn time	103 sec
Propellant	Solid
First stage - L-110
Engines	2 Vikas
Thrust	1,600 kN
Specific impulse	300 sec
Burn time	240 sec
Propellant	UDMH + N2O4
Second stage C25
Engines	1 CE-20
Thrust	200 kN (20 Tf)
Specific impulse	450 sec
Burn time	720 sec
Propellant	LOX/LH2
	[edit on Wikidata]

The GSLV-III or Geosynchronous Satellite Launch Vehicle mark III a current launch vehicle development project by the Indian Space Research Organization that got underway in the early-2000s and is now scheduled for its first suborbital test launch of the GSLV booster stage in 2014.^[5] It is intended to launch heavy satellites into geostationary orbit, and will allow India to become less dependent on foreign rockets for heavy lifting.

The rocket is the technological successor to the GSLV, however is not derived from its predecessor. The GSLV MK-1 had a Russian-made cryogenic third stage, this has been replaced with an Indian-built cryogenic stage for the GSLV MK-2. The GSLV MK-3 will have an Indian built cryogenic stage.^[6]^[7]

Vehicle Description

Boosters

The boosters used on the GSLV-III will be the S-200, which is also designated Large Solid Booster, or LSB, which is a solid propellant stage with a mass of 200 tonnes. Two boosters will be used. Each has a diameter of 3.2 metres and a length of 25 metres. Each booster generates 560 tonnes-force (5.50 MN) of thrust at lift-off.^[8]

Core stage

The core stage will be the L-110 restartable liquid stage which has 110 tonnes of liquid propellant and a diameter of 4-metres. It will be the first Indian liquid engine cluster design, and will use two improved Vikas engines, each producing 75 tonnes (735 kN) of thrust. The improved Vikas engine will use regenerative cooling, providing improved weight and specific impulse, compared to earlier rockets.^[8] L110 is one of the heaviest earth storable liquid stages ever developed by ISRO.^[9]

Upper stage

The cryogenic upper stage will be the C-25, powered by the CE-20 engine, fueled by 25 tonnes of LOX+LH2. It will be 4 metres (13 ft) in diameter and 8.2 metres (27 ft) long. The stage will produce 20 tonnes (^{[convert: unit mismatch]}) of thrust.^[10]

Background

The C-25 upper stage of GSLV MK-3 is powered by the CE-20 cryogenic engine. This engine is slated for completion and testing by 2015, it will then be integrated with the C-25 stage and be put through a series of tests. The first C-25 stage will be used on the GSLV MK-3 D-1 mission in early 2017. This mission will put in orbit the GSAT19E communication satellite.^{[citation needed]} Work on the C-25 stage and CE-20 engine for GSLV Mk-3 upper stage was initiated in 2003, the project has been subject to many delays due to problems with ISRO's smaller cryogenic engine the CE-7.5 for GSLV MK-2 upper stage. After completion of CE-20 engine for GSLV MK-3 ISRO plans to start working on CE-60 and CE-100 cryogenic engines for future heavy lift vehicles being planned.^{[citation needed]}

Payload fairing

The payload fairing will have a diameter of 5 metres (16 ft) and a payload volume of 100 cubic metres (3,500 cu ft).^[10]^{[full citation needed]}

History

Development for the GSLV Mk III began in the early 2000s,^{[clarification needed]} with the first launch originally planned for 2009-2010. In the event, several factors have delayed the program, including the "failure of ISRO-developed cryogenic upper stage on April 15, 2010."^[5]

In 2007, wind tunnel tests were completed and vehicle aero-elastic test activities^{[clarification needed]} commenced. The vehicle configuration update was completed. All major facilities including propellant plant, vehicle assembly and integration building, mobile launch pedestal and facilities at work centers have reached^[when?] the final phase of completion.

First batch of light alloy structure and motor case segments were realized at work centers.^[when?] The avionics system designs have been completed and first batch of packages are being realized for qualification. Avionics assemblies layout has been finalized and integration trials for package assembly are being carried out.^{[citation needed]}

A suborbital flight test of the GLSV Mk3 launcher, without its cryogenic third stage, is planned for April 2014. With first flight now scheduled for April 2014; it is likely the first orbital flight will take place in 2016.^{[citation needed]} ISRO would then need several more successful launches to declare the launcher safe for manned flight. First manned flight is unlikely before 2020, possibly 2–3 years later.^[5]

S-200 Static test

The Solid booster S-200 was successfully tested in 24 January 2010. During the test, the S-200 booster was fired for 130 seconds and generated a peak thrust of about 500 tonnes. The performance of the booster was exactly as predicted. Nearly 600 health parameters were monitored during the test and the initial data indicates normal performance. Second successful static test of solid booster S200 conducted at SDSC, SHAR on September 4, 2011.^[11]

L-110 Static test

Indian Space Research Organisation conducted the static test of its liquid core stage (L110) of GSLV Mk III launch vehicle, for 150 seconds at its Liquid Propulsion Systems Centre (LPSC) test facility at Mahendragiri, Tamil Nadu at 16:00 hrs on March 5, 2010.While the test was originally targeted for 200 seconds it was stopped at 150 seconds since a deviation in one of the parameters was observed. Then on 8 September the same year ISRO successfully conducted the second static testing of L110 for 200 seconds .^[9]^[12] Nearly 500 health parameters were monitored during the test and the initial data acquired indicated its normal performance.^[9]

Scheduled launches

Flight	Launch date/time (UTC)	Variant	Launch Pad	Payload	Payload Mass	Result	Note(s)
	Jan 2014 ^[13]	Mk III	Second		Sub orbital Development flight
E1	2017^[14]	Mk III	Second	GSAT-19E^[15]	kg		orbital first operational flight

Comparable rockets

References

^ "The GSLV-III". Indian Space Research Organisation. 2009-12-07. Retrieved 2012-11-23.
^ "Fresh GSLV launch attempt in July". Indian Express. 2013-04-09. Retrieved 2013-04-09.
^ "India to test world's third largest solid rocket booster". Science and Technology Section. The Hindu News Paper. 2009-12-07. Retrieved 2009-12-07.
^ "LPSC Handouts at Aer India-2009". Specifications of CE-20. Liquid Propulsion Systems Centre. 2009-03-13. Retrieved 2009-08-29.
^ ^a ^b ^c "India's GSLV Mk-3 First Flight Pushed Back to April 2014". Sawfnews.com. 2013-04-05. Retrieved 2013-04-28. The launcher was initially expected to become operational by 2010/2011 with first flight in 2009-10.
^ "Indian Space Research Organisation preparing for three more PSLV launches". English: The Hindu. 2011-04-29. Retrieved 15 July 2011.
^ http://www.spaceref.com/news/viewsr.rss.spacewire.html?pid=38419
^ ^a ^b "Space Transportation". GSLV - Mk III - Status of CE-20. Indian Space Research Organization. 2009-07-15. Retrieved 2009-09-15.
^ ^a ^b ^c ISRO Press Release:Successful Static Testing of L 110 Liquid Core Stage of GSLV - Mk III
^ ^a ^b "Space Transportation". GSLV - Mk III - Status of CE-20. Indian Space Research Organization. 2009-07-15. Retrieved 2009-09-05.
^ Isro successfully tests world's 3rd largest solid booster
^ ISRO successfully conducts static testing of new age rocket
^ http://www.thehindu.com/sci-tech/technology/heaviest-rocket-launch-in-2014-isro/article4602878.ece
^ http://www.frontline.in/science-and-technology/in-mission-mode/article4945199.ece?homepage=true#test
^ http://www.indiantelevision.com/headlines/y2k13/mar/mar109.php

External links

Template:Indian launch systems

[isro20120812-1] "The GSLV-III". Indian Space Research Organisation. 2009-12-07. Retrieved 2012-11-23.

[indianexpress-2] "Fresh GSLV launch attempt in July". Indian Express. 2013-04-09. Retrieved 2013-04-09.

[3] "India to test world's third largest solid rocket booster". Science and Technology Section. The Hindu News Paper. 2009-12-07. Retrieved 2009-12-07.

[4] "LPSC Handouts at Aer India-2009". Specifications of CE-20. Liquid Propulsion Systems Centre. 2009-03-13. Retrieved 2009-08-29.

[sawf20130405-5] "India's GSLV Mk-3 First Flight Pushed Back to April 2014". Sawfnews.com. 2013-04-05. Retrieved 2013-04-28. The launcher was initially expected to become operational by 2010/2011 with first flight in 2009-10.

[6] "Indian Space Research Organisation preparing for three more PSLV launches". English: The Hindu. 2011-04-29. Retrieved 15 July 2011.

[7] ttp://www.spaceref.com/news/viewsr.rss.spacewire.html?pid=38419

[Space_Transportation-8] "Space Transportation". GSLV - Mk III - Status of CE-20. Indian Space Research Organization. 2009-07-15. Retrieved 2009-09-15.

[isro_press_release-9] ISRO Press Release:Successful Static Testing of L 110 Liquid Core Stage of GSLV - Mk III

[isro.org-10] "Space Transportation". GSLV - Mk III - Status of CE-20. Indian Space Research Organization. 2009-07-15. Retrieved 2009-09-05.

[11] Isro successfully tests world's 3rd largest solid booster

[5-12] ISRO successfully conducts static testing of new age rocket

[13] ttp://www.thehindu.com/sci-tech/technology/heaviest-rocket-launch-in-2014-isro/article4602878.ece

[14] ttp://www.frontline.in/science-and-technology/in-mission-mode/article4945199.ece?homepage=true#test

[15] ttp://www.indiantelevision.com/headlines/y2k13/mar/mar109.php

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v t e Orbital launch systems
List of orbital launch systems Comparison of orbital launch systems
Current	Angara 1.2 A5 Ariane 6 Atlas V Ceres 1 1S Chollima-1 Electron Falcon 9 Block 5 Falcon Heavy Firefly Alpha Gravity-1 GSLV H-IIA H3 Hyperbola-1 Jielong 1 3 KAIROS^† Kaituozhe 2 Kinetica 1 Kuaizhou 1 1A 11 Long March 2C 2D 2F 3A 3B/E 3C 4B 4C 5 5B 6 6A 7 7A 8 11 11H LVM3 Minotaur I IV V C Nuri OS-M1^† Pegasus XL Proton-M PSLV Qaem 100 Qased RS1^† Shavit 2 Simorgh SLS Block 1 Soyuz-2 2.1a / STA 2.1b / STB 2-1v SSLV Starship Tianlong-2 Unha Vega C Vulcan Centaur Zhuque 2
In development	Antares 330 Bloostar Cyclone-4M Deca Epsilon S Eris Gravity-2 Hyperbola-2 Irtysh Kuaizhou 21 31 Long March 9 10 12 Miura 5 MLV Neutron New Glenn New Line 1 NGLV Nova OS-M 2 4 Orbex Prime Pallas-1 Red Dwarf SLS Block 1B Block 2 Soyuz-7 Terran R Tianlong-3 VLM Vega E Zero Zhuque 3 Zuljanah
Retired	Antares 110 120 130^† 230 230+ Ariane 1 2 3 4 5 ASLV Athena I II Atlas B D E/F G H I II III LV-3B SLV-3 Able^† Agena Centaur Black Arrow Conestoga^† Delta A B C D E G J L M N 0100 1000 2000 3000 4000 5000 II III IV IV Heavy Diamant Dnepr Energia Epsilon Europa I^† II^† Falcon 1 Falcon 9 v1.0 v1.1 v1.2 "Full Thrust" Feng Bao 1 GSLV Mk I H-I H-II H-IIB Juno I Juno II Kaituozhe-1 Kosmos original 1 2/2I 3 3M Lambda 4S LauncherOne Long March 1 1D^† 2A 2E 3 3B 4A Mu 4S 3C 3H 3S 3SII V N1^† N-I N-II Naro-1 Paektusan^† Pilot-2^† R-7 Luna Molniya M L Polyot Soyuz original FG L M U U2 Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna^† Rocket 3 Safir 1 1A 1B Saturn I IB V Scout X-1 Blue Scout II^† X-2^† X-2M X-3 X-3M X-4 X-2B^† B A B-1 D-1 A-1 E-1 F-1 G-1 Shavit original 1 SLV Space Shuttle SPARK^† Sparta SS-520 Start-1 Terran 1^† Thor Able Ablestar 1 2 Agena A B D Burner 1 2 Delta DSV-2U Thorad-Agena SLV-2G SLV-2H Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Tsyklon R-36-O original 2 3 Universal Rocket UR-500 Proton Proton-K Rokot Strela Vanguard Vega original VLS-1^† Zenit 2 2M 2FG 3SL 3SLB 3F Zhuque 1^†
Classes	Sounding rocket Small-lift launch vehicle Medium-lift launch vehicle Heavy-lift launch vehicle Super heavy-lift launch vehicle
This Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future Symbol ^† indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)