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Context: Recently, ISRO successfully carried out demonstration of restarting its Vikas liquid engine at a test facility at Propulsion Complex, Mahendragiri.
The Vikas engine, a critical component powering the liquid stages of ISRO's launch vehicles, is instrumental in advancing technologies for stage recovery and future launch vehicle reusability.
VIKAS (an acronym for Vikram Ambalal Sarabhai) engine is a family of liquid-fuelled rocket engines conceptualized and designed by the Liquid Propulsion Systems Centre of ISRO in the 1970s.
It has been conceptualized and designed by ISRO’s Liquid Propulsion Systems Centre (LPSC).
LPSC is centre for design, development and realisation of liquid propulsion stages for ISRO's Launch Vehicles.
It is workhorse engine that powers liquid stages of ISRO’s launch vehicles.
These engines are deployed for ISRO’s Polar Satellite Launch Vehicle (PSLV) and the Geosynchronous Satellite Launch Vehicle (GSLV) series of expendable launch vehicles for space launch use.
It improves payload capability of Polar Satellite Launch Vehicle (PSLV), Geosynchronous Launch Vehicle (GSLV) and GSLV Mk-III launch vehicles.
The fuel load of the Vikas engine is 40 tonnes for the PSLV, GSLV Mark I and II, and 55 tonnes for the GSLV Mark III.
First Indian launch vehicle to be equipped with liquid stages.
Four stage vehicle with multiple satellite launch capability and multiple orbit capability. Second and fourth stages are powered by liquid propulsion engines.
Second stage is powered by a Vikas engine. It uses UDMH (Unsymmetrical Dimethyl Hydrazine) as fuel and Nitrogen tetroxide (N2O4) as oxidiser.
Three stage vehicle used to launch communication satellites in geo transfer orbit using cryogenic third stage.
Its second stage is powered by Vikas engines.
By: Shubham Tiwari ProfileResourcesReport error
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