DEVELOPMENT TESTS OF RD815 ENGINE PREBURNER DEMONSTRATOR

Paper number

IAC-19,C4,1,6,x50646

Author

Mr. Alexandr Prokopchuk, Ukraine, Yuzhnoye State Design Office

Coauthor

Mr. Volodymyr Shulga, Ukraine, Yuzhnoye State Design Office

Coauthor

Mr. Andrew Kukhta, Ukraine, Yuzhnoye State Design Office

Coauthor

Mr. Yevgen Strelchenko, Ukraine, Yuzhnoye State Design Office

Year

2019

Abstract

Yuzhnoye State Design Office specialists have developed a project of an intended for launch vehicle first stages RD815 main liquid rocket engine with a sea level thrust of ~250 tf. The engine operates on LOX+kerosene propellants and utilizes a closed cycle.
Experimental fire tests of a demonstrator unit are being undertaken to verify the technical solutions, applied in the design of one of key engine units – the preburner.
The report presents an overview of carried out works and RD815 engine preburner demonstrator test results.

Abstract document

IAC-19,C4,1,6,x50646.brief.pdf

Manuscript document

IAC-19,C4,1,6,x50646.pdf (🔒 authorized access only).

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