SCE-200
Type: Lower Stage Engine
Country of Origin: India
Manufacturer: Godrej Aerospace
First Flight:
Status: In development
Propellant (O/F): Liquid Oxygen/Kerosene
Mixture Ratio (O/F by mass):
Cycle: Staged Combustion
Chambers: 1
Thrust (vac.): 2030 kN
Thrust (s.l.): 1820 kN
Throttle: none
ISP (vac.): 335 s
ISP (s.l.): 299 s
Chamber Pressure: 2610 psi
Nozzle Ratio:
Burn time:
Ignitions:
Mass: 2700 kg
Length:
Diameter:
Used in: ULV
Links: