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The SSLV was developed with the aim of launching small satellites commercially at drastically reduced price and higher launch rate compared to Polar Satellite Launch Vehicle (PSLV). The development cost of SSLV is ₹ 169.07 crore (equivalent to ₹ 190 crore or US$22 million in 2023) [ 16 ] [ 2 ] and the manufacturing cost is expected to be ...
PSLV-XL is the upgraded version of Polar Satellite Launch Vehicle in its standard configuration boosted by more powerful, stretched strap-on boosters with 12 tonne propellant load. [50] Weighing 320 t (310 long tons; 350 short tons) at lift-off, the vehicle uses larger strap-on motors (PSOM-XL or S12) to achieve higher payload capability. [ 89 ]
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 family of three launchers was previously being designed for replacing the different core propulsion modules of PSLV, GSLV, and LVM3 respectively with a common semi-cryogenic engine and hence it was named as Unified Launch Vehicle (ULV). [12] Unlike the latest proposal of the launcher, the initial proposals were planned to be expendable ...
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 ]
All four SLV launches occurred from the SLV Launch Pad at the Sriharikota High Altitude Range.The first two launches were experimental (E) and the next 2 were designated as developmental (D) as this was the first launch vehicle being developed by India not intended for a long service life.
Falcon 9 Block 5, the most prolific active orbital launch system in the world.. This comparison of orbital launch systems lists the attributes of all current and future individual rocket configurations designed to reach orbit.
The electronics in SSLV-D2 worked successfully, as did the launch vehicle's new, affordable guidance and navigation system. [14] D3: 16 August 2024 03:47 [15] [16] SSLV First: EOS-08 SR-0 DEMOSAT 175.5 kg 0.2 kg Total = 175.7 kg LEO: ISRO: Success Third developmental flight and completion of SSLV Development Project.