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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The flight was scheduled for 19 Augustbut one hour and 14 minutes before the lift off, a leakage was reported and the launch was halted.

Retrieved 14 August In other projects Wikimedia Commons. Retrieved 10 February Medium Lift Launch System.

You agree that we have no liability for any damages. The cryogenic rocket engine provides more thrust than conventional liquid rocket engines but the fuel and oxidizer needs to be super dkfference in order to keep them in a liquid state.

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The digital auto-pilot and closed loop guidance scheme ensure the required altitude maneuver and guide injection of the spacecraft to the specified orbit. Retrieved April 27, Archived from the original on March 14, Retrieved 21 December Retrieved 30 March Archived from the original on 4 January Retrieved 1 July Retrieved 22 September I configuration was launched on 18 April was a failure as the payload failed to reach the intended orbit parameters.


Developmental flight, payload placed into lower than planned orbit, and did not have sufficient fuel to reach a usable orbit. Archived from the original on 11 February Retrieved 11 July Satellite is fully operational and full design life of ten years will be achieved. The Times Of India.

I have used Russian cryogenic engines. I is propelled using a Russian made KVD Retrieved November 27, From Wikipedia, the free encyclopedia. It has a diameter of 2.

Geosynchronous Satellite Launch Vehicle

Retrieved 9 January List of orbital launch systems Comparison of orbital launch systems. Retrieved from ” https: The main reason behind the advent of the GSLV is the capability to lift dicference loads into space.

Retrieved 1 April It completed 6 years in orbit successfully. Archived from the original PDF on 16 February Spaceflight portal India portal. Archived from the original on 9 August II [ edit ]. Although the strap-on rockets of the GSLV provide slightly less thrust than those on the PSLV, they burn three times longer and provide greater assistance to the first stage.

Apogee lower and inclination higher than expected, due to an error in the guidance subsystem. Retrieved 20 January Indian satellite launch vehicle. Retrieved 27 April Madhavan Nair 10 September Archived from the original on March 1, This variant uses an Indian cryogenic engine, the CE The Geosynchronous Satellite Ddifference Vehicle GSLV project was initiated in with the objective of acquiring an Indian launch capability for geosynchronous satellites.


What is the difference between SLV, GSLV, PSLV AND ASLV

The injection parameters were met with extreme precision. The third stage was to be procured from Russian company Glavcosmoshetween transfer of technology and design details of the engine based on an agreement signed in Get New Comparisons in your inbox: PSLV is a four-staged launch vehicle with first and third stage using solid rocket motors and second and fourth stages using liquid rocket engines.

Archived from the original on March 18, Difference remote sensing satellites orbit the earth from pole-to-pole at about 98 deg orbital-plane inclination.

Views Read Edit View history. Madhavan Nair 25 July The GSLV also has strap-on rockets but there are only 4 of them and they have liquid fuel. All subsequent launches have used enhanced propellant loaded S stage.