Geosynchronous Satellite Launch Vehicle abbreviated as GSLV, is an expendable launch GSLV uses major components that are already proven in the Polar Satellite Launch Vehicle (PSLV) launchers in the form of the S/S solid rocket . The difference between expected and actual inclination degree was 0. SLV that stands for Satellite Launch Vehicle, was a project started by the Indian Space Research Organisation (ISRO) and was headed by APJ. GEOSYNCHRONOUS SATELLITE LAUNCH VEHICLE(GSLV) About the Launch Vehicle. newer improved version with a higher chamber pressure is used here. The stage was derived from the PS2 of PSLV where the Vikas engine has.

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Perigee was within m within 0. From Wikipedia, the free encyclopedia. The difference between expected and actual inclination degree was 0.

Question corner: What is the difference between GSLV and PSLV?

The GS2 stage is powered by the Vikas engine. This variant uses an Indian cryogenic engine, the CE User assumes all risk of use, damage, or injury.

Developmental flight, payload placed into lower than planned orbit, and did not have sufficient fuel to reach a usable orbit. Retrieved 15 July Retrieved 22 September Retrieved 21 December Retrieved 29 March Archived from the original on Medium Lift Launch System.


Difference Between PSLV and GSLV | Difference Between | PSLV vs GSLV

Archived from the original on 11 February Retrieved 13 December The Geosynchronous Satellite Launch Vehicle GSLV project was initiated in with the objective of acquiring an Indian launch capability for geosynchronous satellites. It has a diameter of 2. Apart from launching the remote sensing satellites to Sun-synchronous polar orbits, the PSLV is also used to launch the satellites of lower lift-off mass of up to about Kg to the elliptical Geosynchronous Transfer Orbit GTO.

The second developmental flight replaced the S stage with S In other projects Wikimedia Commons. Retrieved 15 January Indian satellite launch vehicle. The launcher was declared operational after the second development flight successfully launched the GSAT-2 satellite.

Geosynchronous Satellite Launch Vehicle

Get New Comparisons in your inbox: Retrieved 20 January It is discarded when the vehicle reaches an altitude of about km. Madhavan Nair 25 July betwsen Comprehensive Orbital Launch Failure List”.

During the initial years from the initial launch to the launcher had a checkered history with only 2 successful launches out of 7. The satellite in GTO is further raised to its final destination, viz. Dinesh 31 October All subsequent launches have used enhanced propellant loaded S stage.

Retrieved 27 April The digital auto-pilot and closed loop guidance scheme ensure the required altitude maneuver and guide injection of the spacecraft to the specified orbit. Radhakrishnan attributed the failure to incorrect mixture ratio used an the cryogenic upper stage.


Geosynchronous Satellite Launch Vehicle – Wikipedia

Archived from the original on 26 December Retrieved November 27, Retrieved 11 February I configuration bettween launched on 18 April was a failure as the payload failed to reach the intended orbit parameters. Destroyed by range safety officer after loss of control over liquid-fueled boosters. This article is closed for comments. Views Read Edit View history. With 18 launches, 16 of those fifference successes while only the first one was a total failure; the remaining one is called a partial failure as the satellite did not reach the intended altitude.

Archived from the original on March 14, I is propelled using a Russian made KVD January 01, Retrieved 1 July The cuboid-shaped GSAT-6 satellite includes a technology demonstrator Gspv unfurlable antenna with a diameter of six metre which will provide S-band communication services during its expected mission life of nine years. Retrieved 15 December The chamber pressure in all liquid engines were enhanced, enabling a higher propellant mass and burn time.

The payload fairing, which is 7.

Archived from the original PDF on 5 March Retrieved 1 April Archived from the original on March 1, Archived from the original on 6 January