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This was the first developmental flight of the GSLV Mk.I featuring Russian cryogenic engine KVD-1.It was used to place an experimental satellite GSAT-1 into the orbit. . However, due to sub-optimal performance and lack of fuel the vehicle did not achieve the intended orbit and the satellite had to maneuver itself using onboard fuel to correct the sho
The Geosynchronous Satellite Launch Vehicle (GSLV) project was initiated in 1990 with the objective of acquiring an Indian launch capability for geosynchronous satellites. [ 8 ] [ 9 ] GSLV uses major components that are already proven in the Polar Satellite Launch Vehicle (PSLV) launch vehicles in the form of the S125/S139 solid rocket booster ...
This launch vehicle is an 3-stage launch vehicle. The first stage of GSLV was also derived from the PSLV's PS1. The 138 tonne solid rocket motor is augmented by 4 liquid strap-ons which is lowered by a Vikas rocket engine. GSLV-F15 payload fairing is a metallic version with a diameter of 3.4 meters. [1] [6]
The Launch Vehicle Mark-3 or LVM3 [1] [14] [15] (previously referred as the Geosynchronous Satellite Launch Vehicle Mark III or GSLV Mk III) [a] is a three-stage [1] medium-lift launch vehicle developed by the Indian Space Research Organisation (ISRO).
ISRO's launch vehicles. Left to right: SLV, ASLV, PSLV, GSLV, LVM3 RLV Human Rated Launch Vehicle (HRLV) Vikram series, the under development orbital class launch family of Skyroot Aerospace in comparison with already flown Vikram S, the sounding rocket
This also marks the 15th time that Geosynchronous Satellite Launch Vehicle will be launching the Satellites. This Launch Vehicle is an 3 Stage Launch Vehicle. The first stage of GSLV was also derived from the PSLV's PS1. The 138 tonne solid rocket motor is augmented by 4 liquid strap-ons which is Powered by Vikas (rocket engine).
Launch mass: 2,232 kilograms (4,921 lb) Start of mission; ... NVS-01 was successfully launched by 15th flight of GSLV (GSLV-F12) in Mk2 configuration on 29 May 2023 ...
The CE-7.5 is a cryogenic rocket engine developed by the Indian Space Research Organisation to power the upper stage of its GSLV Mk-2 launch vehicle. The engine was developed as a part of the Cryogenic Upper Stage Project (CUSP). It replaced the KVD-1 (RD-56) Russian cryogenic engine that powered the upper stage of GSLV Mk-1. [3]