RD-0124 (14D23)
Rocket-motor-RD-0124-Salon-du-bourget-2013-DSC 0055.jpg
Country of originRussia
First flight2006-12-27
DesignerKBKhA (Chief designers: Valery Kozelkov, Viktor Gorokhov [ru])[1]
ManufacturerKBKhA in-house[2]
ApplicationUpper Stage
Associated LVSoyuz-2, Soyuz-5
StatusIn Production
Liquid-fuel engine
PropellantLOX / RP-1
CycleStaged Combustion
Thrust, vacuum294.3 kN (66,200 lbf)
Thrust-to-weight ratio52.5
Chamber pressure15.7 MPa (2,280 psi)
Specific impulse, vacuum359 s (3.52 km/s)
Burn time300 s
Length1,575 mm (62.0 in)
Diameter2,400 mm (94 in)
Dry weight572 kg (1,261 lb)
Used in
Soyuz-2-1b and Soyuz-2-1v Block-I

The RD-0124 (GRAU Index 14D23) is a rocket engine burning liquid oxygen and kerosene in a staged combustion cycle. RD-0124 engines are used on the Soyuz-2.1b and Soyuz-2-1v. A slight variation of the engine, the RD-0124A, is used on the Angara rocket family URM-2 upper stage. RD-0124 is developed by Chemical Automatics Design Bureau in Voronezh.[3]


RD-0124 engines use a multi-stage turbopump powered by pre-combustion of the engine propellants in the preburner. The kerosene fuel is used for regenerative cooling of the engine. Vehicle attitude control during ascent is provided by gimbaling the engine in two planes. The propellant tanks are helium-pressurized.[7] Four combustion chambers are fed by a single turbopump system.[7][8] The engine operates at a high chamber pressure and, for the type of propellants used, achieves a very high specific impulse of nearly 360 seconds in vacuum – a specific impulse that can only be exceeded by hydrolox rockets like the RS-25, and by the next-generation methalox rockets like the Raptor engine.


The inaugural flight of a launch vehicle using an RD-0124 engine took place on December 27, 2006.[7] Orbital Sciences considered using the RD-0124 in the High Energy Second Stage (HESS) for their Antares rocket. It would have replaced the Castor 30B second stage.[9]


This upper stage engine has been adapted to two different launch vehicles, the Soyuz-2-1b/v and the Angara family. As such, there are different versions:

See also


  1. ^ ru:Горохов, Виктор Дмитриевич Viktor Gorokhov / ru.wikipedia.org
  2. ^ Люди и ракетные двигатели [People and Rocket Engines: Official History of KBKhA] (in Russian). p. 262.
  3. ^ a b c d "RD0124 (14D23). Launch vehicle "Soyuz-2-1б". RD0124A. "Angara" launch vehicle". KBKhA. Archived from the original on 15 August 2015.
  4. ^ "Turbopumps for Gas Generator and Staged Combustion Cycle Rocket Engines" (PDF). AIAA. July 2005. Retrieved 2015-07-22.
  5. ^ "Жидкостный ракетный двигатель РД-0124А" [Liquid rocket engine RD-0124A] (in Russian). Khrunichev. Archived from the original on 22 July 2015.
  6. ^ Zak, Anatoly. "RD-0110". russianspaceweb.com. Retrieved 2015-07-22.
  7. ^ a b c "The Modernized Soyuz". Starsem. Archived from the original on 8 May 2001.
  8. ^ "Soyuz Overview". Arianespace. Archived from the original on 27 November 2015.
  9. ^ Bergin, Chris (2013-03-05). "CASTOR 30XL prepares for static fire ahead of providing Antares boost". NASA Spaceflight. Retrieved 2015-07-22.
  10. ^ "Двигатель РД0124ДР (дросселированный)" [Engine RD0124DR (throttleable)] (in Russian). KBKhA. Archived from the original on 4 December 2013.
  11. ^ "Двигатель РД0125А" [Engine RD0125A] (in Russian). KBKhA. Archived from the original on 4 December 2013.
  12. ^ "Russian designers have started creating an engine for the Sunkar rocket (In Russian)". TASS. 7 April 2017.