CE-20
Type: Upper Stage Engine
Country of Origin: India
Manufacturer: Hindustan Aeronautics Limited
First Flight:
Status: Active
Propellant (O/F): Liquid Oxygen/Liquid Hydrogen
Mixture Ratio (O/F by mass): 5.05
Cycle: Gas Generator
Thrust (vac.): 200 kN
Thrust (s.l.):
Throttle: 90% to 110%
ISP (vac.): 442.5 s
ISP (s.l.):
Chamber Pressure: 870 psi
Nozzle Ratio: 100
Burn time: 720 sec.
Mass: 0.588 tons
Length:
Diameter:
Used in: LVM3
Links: