Merlin (rocket Engine) - Merlin 1C Engine Specifications

Merlin 1C Engine Specifications

Current published ratings for Merlin 1C variant:

  • Sea level thrust: 556 kN (125,000 lbf)
  • Vacuum thrust: 616 kN (138,400 lbf)
  • Chamber pressure: 6.77 MPa (982 psi)
  • Sea level specific impulse: 275 s (2.6 kN·s/kg)
  • Vacuum specific impulse: 304 s (3.0 kN·s/kg)
  • Thrust-to-weight ratio (fully accounted): 96
  • Fuel: RP-1 (rocket grade kerosene)
  • Oxidizer: liquid oxygen

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