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Д.А. Ягодников, А.В. Сухов, Н.Я. Ирьянов

8

Инженерный журнал: наука и инновации

# 12·2016

Methodological support and calculation

of operational parameters of experimental testing

of model rocket-ramjet engines

© D.A. Yagodnikov, A.V. Sukhov,

N.Ya.

Iryanov

Bauman Moscow State Technical University, Moscow, 105005, Russia

The objective of this project was to develop a calculating technique for ensuring neces-

sary operational parameters of pneumohydraulic system of a bench complex for testing

model rocket-ramjet engines. We solved this problem by using a fire air heater simulating

the conditions on entering the afterburner. The conditions were similar to those in the

flight. We developed sets of equations and performed thermodynamic calculations of the

working body structure produced by a heating gas generator at kerosene combustion in

the air and oxygen regeneration by additional oxygen consumption directly in front of the

afterburner. We obtained the equilibrium temperature values and the values of relative

mass concentration of combustion products. The values are necessary for determining

the operational parameters of the bench equipment and analysis of the experimental data

obtained at fire bench tests.

Keywords:

rocket-ramjet engine, testing, operational parameters, heated air, oxygen

concentration, thermodynamic calculation.

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Yagodnikov D.A.

(b. 1961) graduated from Bauman Moscow Higher Technical School

in 1984. Dr. Sci. (Eng.), Professor, the Head of the Department of Rocket Engines, Bau-

man Moscow State Technical University. Author of over 220 scientific works in the field

of experimental and theoretical research into operation and development of contactless

methods for rocket and jet engine diagnostics. e-mail:

daj@bmstu.ru

Sukhov A.V.

(b. 1937) graduated from Bauman Moscow Higher Technical School in

1961. Dr. Sci. (Eng.), Professor of the Department of Rocket Engines, Bauman Moscow

State Technical University. Author of over 100 scientific works in the field of burning of