Analytical study of control devices for high amplitude combustion instability Quarterly report [PDF]
Mathematical model and analysis of combustion processes in annular rocket engines for control of high amplitude combustion ...
Burstein, S. Z., Schechter, H.
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Rocket propellant injector Patent [PDF]
Propellant injectors for rocket combustion ...
Mantler, R. L.
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Combustion instability research Summary report, 1970 [PDF]
Combustion instability in liquid rocket ...
Bracco, F. V. +9 more
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Investigation of the existing methods for designing pre-combustion chambers in hybrid rocket engines
Hybrid propellant rocket engines (HPRE) have been under development and advancement since the beginning of rocket propulsion research, alongside liquid and solid propellant rocket motors.
Maurício Sá Gontijo
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The paper presents the description of a mathematical model of the working process of a low-thrust rocket engine operating on gaseous oxygen-hydrogen fuel and some fragments of the technology of computational analysis of distribution of gas-dynamic ...
V. V. Ryzhkov, I. I. Morozov
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Overview of Al-based nanoenergetic ingredients for solid rocket propulsion
The introduction of nano-sized energetic ingredients first occurred in Russia about 60 years ago and arose great expectations in the rocket propulsion community, thanks to the higher energy densities and faster energy release rates exhibited with respect
Luigi T. DeLuca
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Summary of combustion instability research at Princeton University, 1969 [PDF]
Control and causes of combustion instability in rocket ...
Bracco, P. V. +11 more
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Nonlinear Aspects of Combustion Instability in Liquid Propellant Rocket Motors. Second Yearly Progress Report for the Period 1 June 1961 to 31 May 1962 [PDF]
Combustion instability in liquid-propellant rocket ...
Harrje, D. T. +2 more
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Oscillatory combustion in rockets Third semiannual report, Jun. 1 - Nov. 30, 1965 [PDF]
Rocket engine oscillatory combustion ...
Goluba, R. +5 more
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Control of transverse instability in rocket combustors Patent [PDF]
Rocket combustion chamber stability by controlling transverse instability during propellant ...
Feiler, C. E., Heidmann, M. F.
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