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The first GSLV flight, GSLV-D1 used the L40 stage. Subsequent flights of the GSLV used high pressure engines in the strap-on boosters called the L40H. [17] The GSLV uses four L40H liquid strap-on boosters derived from the L37.5 second stage, which are loaded with 42.6 tons of hypergolic propellants (UDMH and N 2 O 4). The propellants are stored ...
CE-20 is the first cryogenic engine developed by India which uses a gas generator, as compared to the staged combustion engines used in GSLV. [53] In LVM3-M3 mission, a new white coloured C25 stage was introduced which has more environmental-friendly manufacturing processes, better insulation properties and the use of lightweight materials. [54]
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 GSLV F12 is the 15th flight of the GSLV and the 9th flight of Mk2 variant using indigenous ... Launch of GSLV F12 / NVS 01 Mission is Tentatively Scheduled for ...
Launch of the Chandrayaan-3 lunar exploration mission. 35 2 September 2023 PSLV-XL: C57: Success Launch of the Aditya-L1 scientific mission 36 17 February 2024 GSLV Mk II: F14: Success Launch of the INSAT-3DS weather satellite 37 29 January 2024 GSLV Mk II: F15: Success Launch of the NVS-02 / IRNSS-1K navigation satellite.
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The descent and soft-landing were to be performed by the on-board computers on Vikram, with mission control unable to make corrections. [148] The initial descent was considered within mission parameters, passing critical braking procedures as expected, but the lander's trajectory began to deviate at about 2.1 km (1.3 mi) above the surface.
GSLV F08 launch from SLP. GSLV-F08 carrying GSAT-6A spacecraft was launched from Second Launch Pad of Satish Dhawan Space Centre on 29 March 2018, 11:26 UTC and after flight of 17 minutes 45 seconds, [10] placed GSAT-6A into its planned geostationary transfer orbit with 36,692.5 kilometres (22,799.7 mi) apogee, 169.4 kilometres (105.3 mi) perigee and orbital inclination of 20.64°.