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The GSLV can place approximately 5,000 kg (11,000 lb) into an easterly low Earth orbit (LEO) or 2,500 kg (5,500 lb) (for the Mk II version) into an 18° geostationary transfer orbit. Strap-on motors of GSLV-F05 being integrated with the core stage
Liftoff of GSLV Mk. II F14 from Satish Dhawan Space Centre, carrying INSAT-3DS. This is a list of launches conducted by the Indian Space Research Organisation (ISRO) using Geosynchronous Satellite Launch Vehicle (GSLV) rockets. This list does not include LVM 3 (formerly known as GSLV Mk III) launches, which can be found here.
The GSLV-F15, carrying the NVS-02 satellite, lifted off from the spaceport's second launch pad at 06:23 IST. The satellite was injected into a geostationary transfer orbit (GTO) 19 minutes after launch from Sriharikota. [2] [3] [4] It was the First mission undertaken by newly appointed ISRO chairman Dr. V Narayanan. [5]
The GSLV F12 is the 15th flight of the GSLV and the 9th flight of Mk2 variant using indigenous Cryogenic engine. [1] [2] Launch. Launch of GSLV F12 / NVS 01 Mission ...
GSLV Mk III: Active Upper LH 2 / LOX: Gas generator: 434: 196,500: 60.00: 588: 34.1: 5.05: CE-7.5 India: LPSC: GSLV Mk II: Active Upper LH 2 / LOX: Staged: 454 [6] 73,500: 58: 445: 16.85: E2 USA: ABL Space Systems: RS1: Active 1st RP-1 / LOX // Jet-A / LOX Gas generator: 53,800 [7] 64 E2 Vacuum USA: ABL Space Systems: RS1: Active 2nd RP-1 / LOX ...
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]
The satellite was originally scheduled to be launched from India aboard a GSLV Mark II on 30 March 2024, but it was postponed until further notice due to a needed hardware update. [17] The orbit will be a sun-synchronous, dawn-to-dusk type. The planned mission life is three years. [1]
Geosychronous Satellite Launch Vehicle (GSLV) GSLV Mark I – Retired; GSLV Mark II – Operational; RLV TD: GSLV derived ascent vehicle for RLV ORE campaign. [5] [6] [7] Launch Vehicle Mark III (LVM-3) LVM 3 – Operational; Human-rated LVM 3 – Under development; LVM 3 with semi-cryogenic engine – Under development