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Merlin 1Dvac
Part of Merlin
SpaceX LOx/Kerosene rocket engine. Hardware. Version of the Merlin 1D for upper stage use, with an expansion nozzle greater than 117 resulting in a specific impulse said to be 340 seconds but probably even greater based on the vehicle performance.

AKA: Merlin 1D. Status: Hardware. Date: 2013-. Thrust: 801.00 kN (180,071 lbf). Gross mass: 550 kg (1,210 lb). Specific impulse: 348 s. Specific impulse sea level: 0 s. Burn time: 370 s.

Propellant Formulation: Lox/RP-1. Chamber Pressure: 96 bar. Area Ratio: 120. Thrust to Weight Ratio: 150.

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