RD-0146
The RD-0146 is a Russian cryogenic rocket engine. The RD-0146 engine was developed by KBKhA design bureau in Voronezh, Russia, in cooperation with the American Pratt & Whitney Rocketdyne company. In 2009, it came into prominence, as Russian space agency chose it for the second-stage of the proposed Rus-M launch vehicle designed to carry the future Russian PPTS crewed spacecraft.[1] After the cancellation of Rus-M rocket, the RD-0146D variant was selected as the powerplant for the KVTK upper stage.
Model of RD-0146 | |
Country of origin | Russia |
---|---|
Date | 2001 |
Designer | KBKhA Design Bureau |
Manufacturer | TsSKB Progress |
Application | engine for KVTK upper stage |
Liquid-fuel engine | |
Propellant | LOX / LH2 |
Cycle | Expander cycle |
Configuration | |
Chamber | 1 |
Performance | |
Thrust (vac.) | 68.6 kN (15,400 lbf) |
Chamber pressure | 5.9 megapascals (860 psi) |
Isp (vac.) | 470 seconds (4.6 km/s) |
Dimensions | |
Length | 3.558 metres (11.67 ft) |
Diameter | 1.95 metres (6 ft 5 in) |
Development
In 1999, Khrunichev requested KBKhA to develop RD-0146U version of the engine for Proton and Angara rockets. The development of the engine was partially financed by Pratt & Whitney Rocketdyne. Pratt & Whitney signed a preliminary marketing agreement on April 7, 2000 with Russia's Chemical Automatics Design Bureau giving Pratt & Whitney exclusive international marketing rights to the RD-0146.[1]
Description
The RD-0146 is the first Russian rocket engine not to feature a gas generator and to be equipped with extendable nozzle extension without a cooling system. The engine is capable of five firings and thrust control in two planes. According to the developer, the lack of a gas generator system ensures higher reliability of the engine for multiple firings, by removing the potential of an ignition failure in the engine power cycle.
See also
References
External links
- KBKhA RD-0146
- RD-0146 Specifications
- RD-0146 description from Pratt & Whitney Rocketdyne