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
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Engine modifications
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| 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).