Merlin 1C

Type: Lower Stage Engine and Upper Stage Variant
Country of Origin: United States
Manufacturer: SpaceX

First Flight: August 3, 2008
Status: Retired
Propellant (O/F): Liquid Oxygen/Kerosene
Mixture Ratio (O/F by mass):
Cycle: Gas-Generator
Chambers: 1

Thrust (vac.): 480 kN; 411 kN?? (1C Vacuum)
Thrust (s.l.): 420 kN
Throttle:
ISP (vac.): 304.8 s; 342 s (1C Vacuum)
ISP (s.l.): 275 s
Chamber Pressure: 982 psi
Nozzle Ratio:
Burn time:
Ignitions: 1

Mass: 1380 kg (SL)
Length: 2.9 m
Diameter:

Used in: Falcon 1, Falcon 9

Links:

Wikipedia