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RD-869 (РД-869) Country of origin Soviet Union Date 1983-1985 First flight March 1986 Designer Yuzhnoye Design Bureau Manufacturer Yuzhmash Application Upper Stage Associated LV R-36M2 Predecessor RD-864 Status In service Propellant N 2 O 4 / UDMH Mixture ratio 1.8 Cycle Gas generator Chamber 4 Thrust
High thrust mode: 20.47 kN (4,600 lbf)
Low thrust mode: 8.58 kN (1,930 lbf)
Chamber pressure
High thrust mode: 4.1 MPa (590 psi)
Low thrust mode: 1.7 MPa (250 psi)
Specific impulse
High thrust mode: 313 seconds
Low thrust mode: 302.3 seconds
Burn time Up to 700 s Restarts 50 Gimbal range ±55° Length 4,020 mm (158 in ) Diameter 1,420 mm (56 in ) Dry weight 196 kg (432 lb ) R-36M2 third stageReferences [1] [5] [6] [10]
The RD-864 (GRAU : 15D177 ) is a Soviet liquid propellant rocket engine burning UDMH and nitrogen tetroxide in a gas generator combustion cycle .[1] It has a four combustion chambers that provide thrust vector control by gimbaling each nozzle in a single axis ±55°. It is used on the third stage of the R-36M UTTKh (GRAU : 15A18 ) and Dnepr .[5] For the R-36M2 (GRAU : 15A18M ), an improved version, the RD-869 (GRAU : 15D300 ) was developed.[1] [6] [10] [11]
History [ edit ]
When the Soviet military developed an improved version of the R-36M ICBM , Yangel 's OKB-586 developed a new engine for the third stage, the RD-864 . Developed between 1976 and 1978 it flew for the first time on October 31, 1977. With the START I and START II the some 150 R-36M and R-36M UTTKh were retired and to be destroyed by 2007.[1] [4] So, a civilian application was looked for and during the 1990s, Yuzhnoe Design Bureau (the R-36M designer) successfully developed the Dnepr launch vehicle .[3] It flew for the first time on April 21, 1999 and as of June 2016 it is still operational.[12] So, while the production of the RD-864 has long since been finished, the engine is still to this day operational.[12] [13]
The RD-869 was an improved version for the most powerful Soviet ICBM ever, the R-36M2 (15A18M). It had improved efficiency, restart capability and burn life over the RD-864.[1] [10] As of January 2016 there are still 46 operational R-36M2 (RS-20V, SS-18) and thus the RD-869 is still in service, if out of production.[13]
Versions [ edit ]
There are two versions of this engine:
RD-864 (GRAU Index: 15D177 ): First developed as the third stage engine for the R-36M UTTKh (15A18) ICBM and, by extension, on the Dnepr launch vehicle .[1] [5]
RD-869 (GRAU Index: 15D300 ): An improved version of the RD-864. It has improved efficiency, restart capability and burn life. It is used on the R-36M2 (15A18M).[1] [6]
See also [ edit ]
R-36M UTTKh - The most powerful ever Soviet ICBM for which the RD-864/869 engines were created.
Dnepr - A Ukrainian small rocket project that uses the RD-864.
Yuzhnoe Design Bureau - The RD-864/869 designer bureau.
Yuzhmash - A multi-product machine-building company that's closely related to Yuzhnoe and manufactures the RD-RD-864/869.
References [ edit ]
^ Brügge, Norbert. "Dnepr Propulsion" . B14643.de. Retrieved 2015-08-06 .
^ a b Wade, Mark. "Dnepr" . Encyclopedia Astronautica . Archived from the original on October 15, 2002. Retrieved 2016-07-07 .
^ a b Wade, Mark. "R-36MU 15A18" . Encyclopedia Astronautica . Archived from the original on November 29, 2010. Retrieved 2016-07-07 .
^ a b c d Wade, Mark. "RD-864" . Encyclopedia Astronautica . Archived from the original on June 26, 2002. Retrieved 2016-07-07 .
^ a b c d Wade, Mark. "RD-869" . Encyclopedia Astronautica . Archived from the original on May 6, 2002. Retrieved 2016-07-07 .
^ Pillet, Nicolas. "Le troisième étage de Dniepr" [The Dnepr third stage] (in French). Kosmonavtika.com. Retrieved 2016-07-07 .
^ "Dnepr" . Yuzhnoye. Archived from the original on 28 October 2014.
^ "Dnepr Launch Vehicle" . Yuzhmash. Archived from the original on 15 December 2012.
^ a b c Wade, Mark. "R-36M2 15A18M" . Encyclopedia Astronautica . Archived from the original on September 10, 2010. Retrieved 2016-07-07 .
^ Pal'kov, V. A.; Timchenko, A. Ju.; Stecenko, A. Ja. (2014). Tkachenko, V. D. (ed.). Шестьдесят лет в ракетостроении и космонавтике. 1954-2014 [Sixty years in rocketry and astronautics. 1954-2014 ] (in Russian). Yuzhnoye SDO. pp. 183–185. ISBN 978-966-348-349-8 .
^ a b Krebs, Gunter Dirk (2016-06-13). "Dnepr" . Gunter's Space Page . Retrieved 2016-07-07 .
^ a b "Strategic Rocket Forces" . January 2016. Retrieved 2016-07-07 .
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