Geosynchronous Satellite Launch Vehicle(GSLV)-Mark I&II ,is capable of placing INSAT–II class of satellites (2000 – 2,500 kg) into Geosynchronous Transfer Orbit (GTO). GSLV is a three stage vehicle GSLV is 49 m tall, with 414 t lift off weight. It has a maximum diameter of 3.4 m at the payload fairing. First stage comprises S125 solid booster with four liquid (L40) strap-ons. Second stage (GS2) is liquid engine and the third stage (GS3) is a cryo stage. The vehicle develops a lift off thrust of 6573 kn. The first flight of GSLV took place from SHAR on April 18, 2001 by launching 1540 kg GSAT-1. It was followed by six more launches , GSLV-D2 on May 8, 2003 (GSAT-2 1825 kg), GSLV-F01 on September 20, 2004 (EDUSAT 1950 kg), GSLV-F02 on July 10, 2006, GSLV-F04 on September 2, 2007 (INSAT-4CR 2130 kg), GSLV-D3 on April 15, 2010 and GSLV-F06 on December 25, 2010. Typical Parameters of GSLV Lift-off weight 414 tonne Pay Load 2 to 2.5 Tonne in to Geosynchronous Transfer Orbit (GTO) Height 49 metre GSLV Milestones GSLV-F06 launched GSAT-5P on December 25, 2010 (Unsuccessful) GSLV-D3 launched GSAT-4 on April 15, 2010 (Unsuccessful) GSLV-F04 launched INSAT-4CR on September 2, 2007 (Successful) GSLV-F02 launched INSAT-4C on July 10, 2006 (Unsuccessful) GSLV-F01 launched EDUSAT(GSAT-3) on September 20, 2004 (Successful) GSLV-D2 launched GSAT-2 on May 8, 2003 (Successful) GSLV-D1 launched GSAT-1 on April 18, 2001 (Successful)
Posted on: Tue, 05 Nov 2013 16:36:47 +0000
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