Technogeneous impact of rocket and space activities on the environment is one of the most actual problems of practical cosmonautics. This technogeneous impact is not only the pollution of near Earth space with space debris (worked-off stages of space ...
V. Trushlyakov+2 more
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Mathematical model for heat transfer in variable thickness fins for rocket engines
Purpose. This article aims to develop a mathematical model for a fin in the cooling system of liquid propellant rocket engines. The objective is to enable calculations for fins with arbitrary thickness variation. The developed mathematical model will be
Volodymyr Sliusariev, Valerii Bucharskyi
doaj
Discussion: “Liquid-Propellant Rocket Power Plants” (Zucrow, M. J., 1947, Trans. ASME, 69, pp. 847–856) [PDF]
J. H. Wyld
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Simple Learning-Based Robust Nonlinear Control of an Electric Pump for Liquid-Propellant Rocket Engines [PDF]
Mohammad Jafari+2 more
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ADN – The new oxidizer around the corner for an environmentally friendly smokeless propellant [PDF]
The search for a smokeless propellant has encouraged scientists and engineers to look for a chlorine-free oxidizer as a substitute for AP (ammonium perchlorate).
Márcio Y. Nagamachi+3 more
doaj
Radiative Heating in Combustion Chamber of Liquid Propellant Rocket Engines
The effects of radiation heat transfer in rocket engine combustion chambers are studied analytically. The fuel is hydrogen, methane or ethanol, and the oxidizer is oxygen. Radiative heat fluxes are estimated using empirical equations, and convective heat
K. Takeshi, Satoshi Masaki
semanticscholar +1 more source
On possibility to use flow control units of electromagnetic type for liquid propellant rocket engines [PDF]
С. А. Шевченко
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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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Mathematical simulation of choking under self-oscillations in hydraulic systems with cavitating pumps of liquid-propellant rocket engines [PDF]
S.I. Dolgopolov
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Modeling and Simulation of Liquid Propellant Rocket Engine Transient Performance Using Modelica
This paper presents a liquid propellant rocket engine (LPRE) model library in Modelica language, which contains component models such as pipes, valves, tanks, turbo-pumps, combustion chambers, nozzles, injectors, gas generators, etc.
L. Wei+5 more
semanticscholar +1 more source