Vikas (rocket engine)
Indian rocket engine / From Wikipedia, the free encyclopedia
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The Vikas (a portmanteau from initials of VIKram Ambalal Sarabhai[5][6] ) is a family of hypergolic liquid fuelled rocket engines conceptualized and designed by the Liquid Propulsion Systems Centre in the 1970s.[7][8] The design was based on the licensed version of the Viking engine with the chemical pressurisation system.[9] The early production Vikas engines used some imported French components which were later replaced by domestically produced equivalents.[10] It is used in the Polar Satellite Launch Vehicle (PSLV), Geosynchronous Satellite Launch Vehicle (GSLV) and LVM3 for space launch use.
Country of origin | India |
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Designer |
|
Manufacturer | Godrej & Boyce and MTAR Technologies[1] |
Predecessor | Viking |
Status | Active |
Liquid-fuel engine | |
Propellant | N2O4 / UDMH |
Cycle | Gas generator |
Performance | |
Thrust | 850 kN[2] |
Chamber pressure | 6.2 MPa (62 bar) [3][4] |
Specific impulse, vacuum | 293 seconds (2.87 km/s)[3] |
Specific impulse, sea-level | 262 seconds (2.57 km/s)[3] |
Dimensions | |
Length | 3.70 m (12.1 ft)(Vikas-4B) |
Dry weight | 120 in (3,000 mm) |
Used in | |
2nd stage of PSLV and GSLV Main stage L110 of LVM3 |
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.