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.
REFERENCES
[1]
Polezhayev Yu.V., Shishkov A.A.
Gas-dynamic tests of thermal protection
[Gasdynamic tests of thermal protection]. Handbook. Moscow, Promedek Publ.,
1992, 248 p.
[2]
Trusov B.G.
Inzhenernyi zhurnal: nauka i innovatsii — Engineering Journal:
Science and Innovation
, 2012, issue 1. DOI: 10.18698/2308-6033-2012-1-31
[3]
Alexandrov
V.Yu., Arefyev
K.Yu., Prokhorov A.N., Fedotova K.V., Sharov M.S.,
Yanovsky Ya.S.
Izvestiya vysshikh uchebnykh zavedenii. Mashinostroenie —
Proceedings of Higher
Educational Institutions. Machine building
, 2016,
no. 2 (671), pp. 65–75. DOI: 10.18698/0536-1044-2016-2-65-75
[4]
Volkov V.T., Yagodnikov D.A.
Issledovaniya i stendovaya otrabotka RDTT
[Studies and bench testing of solid-propellant rocket engines]. Moscow,
BMSTU Publ., 2007, 296 p.
[5]
Yagodnikov D.A.
Vosplamenenie i gorenie poroshkoobraznykh metallov
[Ignition and combustion of powdery metals]. Moscow, BMSTU Publ., 2009,
436 p.
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.ruSukhov 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