GSLV MK 2

The GSLV Mk II (Geosynchronous Satellite Launch Vehicle Mark II) is an Indian launch vehicle developed by the Indian Space Research Organisation (ISRO) to place communication satellites into high orbits. It's a three-stage rocket that uses an indigenous cryogenic engine for its upper stage and can launch 2-ton class satellites into Geostationary Transfer Orbits (GTO).

Payload Capability: Designed to launch 2-ton class satellites into Geostationary Transfer Orbits.
Height: Approximately 49.13 meters.
Diameter: 3.4 meters.
First Flight: April 18, 2001.
Key Technology: The use of an indigenously developed cryogenic upper stage enhances its thrust and efficiency for orbital insertion.