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Expendable LV's

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Angara
Ariane 4
Ariane 5
Athena
Atlas II
Atlas III
Atlas V
Avrora (Aurora)
Beal BA-2
Delta II
Delta III
Delta IV
Dnepr
Eurockot
GSLV
H-IIA
J-1
Kosmos 3M
Long March 3
Pegasus
Proton
Shtil
Soyuz
Start
Strela
Taurus
Titan II
Titan IV
Tsiklon
Zenit

   GSLV - Summary
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The Geosynchronous Satetllite Launch Vehicle (GSLV) is intended to eventually launch Insat-type satellites for India, to make India less dependent on foreign rockets for Insat launches. The GSLV improves on the performance of the PSLV with the addition of liquid strap-on boosters and a cryogenic upper stage. The solid first and liquid second stages are carried over from the PSLV. The GSLV will initially use a cryogenic upper stage supplied by Russia, having ordered 7 upper stages. India originally tried to buy the technology to build a cryogenic upper stage from Russia, but under pressure from the United States, that technology was not provided. Therefore, India, has been working on developing a cryogenic upper stage for the past seven years.

 

 

The GSLV uses four L40 liquid strap-on boosters and can place approximately 5000 kg (11,000 lbm) into an easterly LEO orbit. Using the Russian KVD-1 cryogenic upper stage, GSLV can place 2200 kg (4,850 lbm) into a 18 degree GTO orbit. 

Prime Contractor: Indian Space Research Organization (ISRO)
Point of Contact Antrix Corporation, Ltd.
Antrix Complex, Near New BEL Road
Bangalore 560-094, India

Tel: +91 - 80 - 341 6273/274

Launch Site: SHAR Center, Sriharikota Island (13.7°N, 80.2°E)
Web Links: ISRO GSLV Web Site

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