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RS-68 ENGINE

Commercially-developed liquid hydrogen booster engine providing nearly 700,000 pounds of thrust.

Pratt & Whitney Rocketdyne's RS-68 engine was designed for the Delta IV family of evolved expendable launch vehicles (EELV) with a liquid-hydrogen and oxygen booster. The bell-nozzle RS-68 design permits a drastic reduction in part count (compared with current cryogenic engines) which directly translates to lower development and production costs.

Photos

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Specs

Propellants
  • Fuel: H2
  • Oxidizer: LOX
Thrust
  • Vacuum: 768 Klbf.
  • Sea Level: 663 Klbf.
Specific Impulse
  • Vacuum: 409 sec.
  • Sea Level: 359 sec.
  • Area Ratio: 22:1
  • Chamber Pressure: 1,488 psia
  • Engine Mixture Ratio: 6.0
Dimensions
  • Length: 205 in.
  • Diameter: 96 in.
  • Weight: 14,875 lb.