The Vikas (a Blend word from initials of Vikram Sarabhai ) is a family of hypergolic conceptualized and designed by the Liquid Propulsion Systems Centre (LPSC) in the 1970s. The design was based on the licensed version of the Viking engine with the chemical pressurisation system. The early production Vikas engines used some imported French components which were later replaced by domestically produced equivalents. It is used in the Polar Satellite Launch Vehicle (PSLV), Geosynchronous Satellite Launch Vehicle (GSLV) and LVM3 for space launch use.
Vikas engine is used to power the second stage of PSLV, boosters and second stage of GSLV Mark I and II and also the core stage of LVM3. The propellant loading for Vikas engine in PSLV, GSLV Mark I and II is 40 tons, while in LVM3 is 55 tons.
For launches from 2018 a 6% increased thrust version of the Vikas engine was developed. It was demonstrated on 29 March 2018 in the GSAT 6A launch second stage. It will be used for the four Vikas engines first stage boosters on future missions.
Booster/first stage | ||||||||||||
Vikas-2 | ~1.00 | ~2.75 | 13.9 | 5.30 | UDMH / | 1.86 | 0.2469 | 600.5 | 680.5 | 2432 | 2756 | GSLV |
Vikas-2B | ~1.00 | ~2.75 | 13.9 | 5.30 | UH 25 / | 1.87 | 0.2710 | 677.7 | 765.5 | 2501 | 2824 | GSLV |
Vikas-X | ~1.80 | ~3.75 | UH 25 / | 0.2805 | 756.5 | 839.0 | 2697 | 2991 | LVM3 L110 stage | |||
Second stage | ||||||||||||
Vikas-4 | ~1.50 | ~3.50 | 5.35 | UDMH / | 1.86 | 0.2498 | - | 725.0 | 2903 | GSLV, PSLV | ||
Vikas-4B | ~1.80 | ~3.70 | 5.85 | UH 25 / | 1.71 | 0.2716 | - | 804.5 | 2962 | GSLV, PSLV | ||
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