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Merlin 1D
Part of Merlin Family
SpaceX LOx/Kerosene rocket engine. Hardware. First stage version of the Merlin developed for the Falcon 9.1. Based on the Merlin 1C and using a regeneratively cooled combustion chamber. First flight 2014.

Status: Hardware. Date: 2013-. Thrust: 716.00 kN (160,963 lbf). Gross mass: 490 kg (1,080 lb). Specific impulse: 311 s. Specific impulse sea level: 282 s. Burn time: 180 s.

Propellant Formulation: Lox/RP-1. Chamber Pressure: 96 bar. Area Ratio: 16. Thrust to Weight Ratio: 150.





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