Semi Cryogenic Engine ISRO

Hello sir I am here as I want to get the information related to Semi Cryogenic Engine-200 of ISRO so will you please provide me the information??

Semi Cryogenic Engine-200 is a liquid-fuel rocket engine being developed by the Liquid Propulsion Systems Centre, a subsidiary of India's space agency ISRO.

It is being developed to power the future heavy-lift Unified Launch Vehicle (ULV) and the Reusable Launch Vehicle (RLV) being planned by ISRO but before that it will be tested with GSLV Mk III by replacing L110(powered by old Vikas engine) stage to SC160.

Information related to SCE-200 is given below:

Designer
LPSC, Indian Space Research Organisation

Manufacturer
Godrej Aerospace,Godrej & Boyce Ltd

Application
Main engine


Liquid-fuel engine

Propellant
LOX / RP-1

Cycle
Staged combustion

Configuration
Chamber 1

Performance

Thrust (vac.) 2,030 kN (460,000 lbf)

Thrust (SL) 1,820 kN (410,000 lbf)

Chamber pressure 18 MPa

Isp (vac.) 335 seconds (3.29 km/s)

Isp (SL) 299 seconds (2.93 km/s)


Dimensions
Dry weight ~2700 kg

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Answered By StudyChaCha Member