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2. Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2018 (2); 8-15

DOI: https://doi.org/10.33136/stma2018.02.008

Language: Russian

Annotation: One of the important directions in the development of Yuzhnoye SDO liquid rocket engines is creation of the engines for launch vehicle upper stages, boosters, space tugs and takeoff-and-landing vehicles. The article presents an overview of Yuzhnoye SDO – developed liquid rocket engines, their basic characteristics, distinctive features and the current status of development and operation. The article presents the information on the following engines: RD858 and RD859 operating on storable propellants, for lunar takeoff-and-landing Block E module; RD809M and RD809K operating on liquid oxygen + kerosene created on the basis of RD8 serial control engine of Zenit launch vehicle second stage. In this case, RD809M engine is RD8 version with tight integration and RD809K engine is its one-chamber version; RD805 engine operating on liquid oxygen + kerosene created on the basis of combustion chamber of RD8 serial control engine of Zenit launch vehicle second stage.; RD835 engine operating on liquid oxygen + kerosene created for the second stages of launch vehicles of Mayak type; the engines and propulsion systems operating on storable propellants, such as RD861K (main engine of Cyclone-4 third stage and Cyclone-4M launch vehicle second stage), DU802 (liquid propulsion system of Krechet autonomous space tug of conversion Dnepr launch vehicle), RD840 (apogee liquid rocket engine of liquid propulsion system of geostationary communication satellite bus), VG143 (main engine assembly of the fourth stage of European Vega launch vehicle), RD864 and RD869 (main engines of Dnepr launch vehicle upper stages). The information presented in the article is of interest to liquid rocket engines and launch vehicles developers.

Key words: main engine, engine development test, takeoff-and-landing module, pneumatic pump unit

Bibliography:
1. Liquid Rocket Engines, Propulsion Systems, Onboard Power Sources Developed by Propulsion Systems Design Office of Yuzhnoye SDO / Under scientific editorship of S. N. Konyukhov, Academician of NAS of Ukraine, V. N. Shnyakin, Candidate of Engineering Science. Dnepropetrovsk, 2008. 466 p.
2. Liquid Rocket Engines. Description and Basic Technical Data / Under scientific editorship of S. N. Konyukhov, Academician of NAS of Ukraine, V. N. Shnyakin, Candidate of Engineering Science. Dnepropetrovsk, 1996. 84 p.
3. Prokopchuk A. A. et al. New Possibilities for Creation of Apogee Propulsion Systems with Pneumopump Propellant Supply System. Paper presentation at Conference “Space Propulsion”, 2018, Spain.
4. Shnyakin V. N., Shulga V. A., Dibrivny A. V. Possibilities of Creating New LRE Based on Mature Technologies. Space Technology. Missile Armaments: Collection of scientific-technical articles. 2011. Issue 2. P. 61-71.
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2.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines
2.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines
2.2.2018 Yuzhnoye SDO-Developed Upper Stage Liquid Rocket Engines

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