The advanced liquid rocket engine line of SDO “Yuzhnoye” for the creation of new families of launch vehicles

1Prokopchuk, AA, 1Shulga, VА
1Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 2015, 21 ;(5):28–35
https://doi.org/10.15407/knit2015.05.028
Section: Space Energy, Power and Propulsion
Publication Language: Russian
Abstract: 

SDO “Yuzhnoye” specialists are working on the creation of advanced liquid rocket engine (LRE) line that first of all, allows satisfying our own needs in modern engines due to creation of new families of launch vehicles (LV) as well as satisfying requirements of the market. The creation of this LRE line allows us to be sure in the independence of Ukrainian rocket industry from foreign shipment of modern LRE for the solving of an independent access to space market that is actual for all the technically developed economics.

Keywords: LOX-kerosene LRE, main LRE, specific thrust impulse, stage combustion cycle, thrust
References: 

1. Degtjarev A.V., Prokopchuk A.A., Shul'ga V.A. et al. Marshevyj dvigatel' RD809K: Jeskiznyj proekt. Vybor parametrov, konstrukcii dvigatelja i osnovnyh agregatov. Pojasnitel'naja zapiska. Ch.1 M22 YZH ANL 036 01. 272 p. (GP «KB «Juzhnoe», Dnepropetrovsk, 2014) [in Russian].

2. Degtyarev A.V., Shulga V.A., Zhivotov A.I., Dibrivny A.V. The development of lox-kerosene liquid rocket engines family for perspective launch vehicles of Yuzhnoye SDO based on proven technologies. Aerospace technic and technology, No.1(98), 44 —50 (2013) [in Russian].

3. Konjuhov S.N., Shnjakin V.N., Shul'ga V.A. et al.. Marshevyj dvigatel' RD809 vtoroj stupeni RN «Turus-2»: Jeskiznyj proekt. Pojasnitel'naja zapiska 00.1506.0000.0000.09.0 PZ. 50 p. (GP «KB «Juzhnoe», Dnepropetrovsk, 2010) [in Russian].

4. Shnyakin V.N., Shulga V.A., Zhivotov A.I., Dibrivny A.V. Space liquid rocket engines with multiple in-flight restarts and thrust regulation. IAC-11.C4.1.9. P.6299-6304 (2011) [in Russian].