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Family: SLV. Country: India. Status: Development. Other Designations: Geostationary Satellite Launch Vehicle.

Indian launcher for geosynchronous satellites using a Lox/LH2 upper stage developed from Russian technology.


LEO Payload: 5,000 kg. to: 200 km Orbit. at: 45.0 degrees. Payload: 2,500 kg. to a: Geosynchronous transfer trajectory. Liftoff Thrust: 694,000 kgf. Total Mass: 402,000 kg. Core Diameter: 2.8 m. Total Length: 49.0 m. Development Cost $: 500.00 million. Launch Price $: 45.00 million. in 1999 price dollars. Flyaway Unit Cost $: 4.00 million. in 1985 unit dollars.


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Last update 12 March 2001.
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