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RD-180

RD-180 engines for a first stage of “Atlas” launch-vehicle

 

            In the beginning 1996 the NPO Energomash’ project of RD-180 engine was recognized as the winner of competition on development and delivery of the engine of a first stage for the upgraded “Atlas” launch-vehicle of the US aerospace company Lockheed Martin. It is the dual-chamber engine with afterburning of oxidizer-rich preburner’ gas, with thrust vector control thanks to gimballing of each chamber in two planes, with a capability to provide deep throttling of engine thrust in flight. The given design bases on the well proven designs of units and parts of RD-170/171 engines. The creation of the powerful engine of a first stage was carried out in the shortest possible time, and development - on small quantity of hardware. Having signed contract on engine development in summer 1996, the first fire test of the engine – prototype was conducted in November 1996, and in April 1997 - fire test of the nominal engine. In 1997-1998 the set of fire tests of the engine in a structure of a stage of the launch-vehicle was successfully conducted in USA. The certification of the engine for use in a structure of “Atlas 3” launch-vehicle was completed in spring 1999. The maiden launch of “Atlas 3” launch-vehicle with RD-180 engine was conducted in May 2000. The certification of the engine for use in a structure of the “Atlas 5” launch-vehicle was completed in summer 2001. The maiden flight of “Atlas 5” launch-vehicle with the RD-180 engine was conducted in August 2002.

Main parameters of RD-180 engine

 

Liquid propellant rocket engine with afterburning of oxidizer-rich gas

Propellant                                               liquid oxygen + kerosene

 

Engine modifications

RD-180


Thrust, sea level / vacuum, tf
390 / 424
Specific impulse, sea level / vacuum, sec
311,3 / 337,8
Combustion chamber pressure, kgf/cm2
272
Weight, dry / filled, kg
5400 / 5850
Overall dimensions, height / diameter, mm
3600 / 3200
Period of development
1994-1999
Purpose

“Atlas III” and “Atlas V”

 

To the present time the contracts on delivery 50 serial production engines are signed, the Lockheed Martin company has declared intention to order not less than 101 engines RD-180 for use in a structure of “Atlas 3” and “Atlas 5” launch-vehicles. For marketing and realization of the given engine to the customer – Lockheed Martin company earlier, ULA now - the RD AMROSS joint venture was created by NPO Energomash and Pratt&Whitney (USA). About 40 serial production engines already are delivered in USA, 18 launches of “Atlas 3” and “Atlas 5” launch-vehicles with RD-180 engines on a first stage are conducted (end of 2007).

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