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RD-180 ENGINE

International cooperation and partnership yielding nearly one million pounds of thrust for the Atlas V fleet.

Packing nearly one million pounds of thrust in a total propulsion system, the RD-180 engine delivers a 10 percent performance increase over Lox/RP booster engines. This reusable kerosene (hydrocarbon)-fueled engine has been flight-proven on the United Launch Alliance Atlas III and Atlas V launch vehicles.

The RD-180 is a two-chamber derivative of the four-chamber RD-170 that was used on Russian vehicles and human-rated in Russia.

It provides an environmentally-clean operation, while featuring an integrated-propulsion package with hydraulics for control-valve actuation and thrust-vector gimbaling, pneumatics for valve actuation and system purging, and a thrust frame to distribute loads.

The RD-180 booster engine is offered by RD AMROSS, a partnership between the world's two premier propulsion companies—Pratt & Whitney Rocketdyne of the U.S. and NPO Energomash of Russia.

Photos

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Specs

Nominal Thrust
  • Vacuum: 933,400 lb.
  • Sea Level: 860,200 lb.
Specific Impulse
  • Vacuum: 339.3 sec.
  • Sea Level: 312.7 sec.
  • Nozzle Area Ratio: 36.4:1
  • Chamber Pressure: 3,772 psia
  • Mixture Ratio: 2.72
  • Throttle Range: 47%–100%
Dimensions
  • Length: 140 in.
  • Diameter: 124 in.
  • Dry Weight:
    12,081 lb. (5,480 kg.)