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  1. 121
    PECULIARITIES OF COOLING COMBUSTION CHAMBER OF ROCKET ENGINE, WHICH UTILIZE HIGH-TEST PEROXIDE AS AN OXIDIZER
    “... combustion chambers.       This article threats peculiarities of cooling combustion chamber of rocket engine...”
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    Article
  2. 122
    THE PROBLEM OF THE OPTIMIZATION THE DESIGN PARAMETERS AND CONTROL PROGRAMS OF THE CONTROLLED ROCKET WITH SOLID PROPELLANT ROCKET ENGINE
    “... of the controlled single-stage rocket with cruise solid propellant rocket engine is formulated. The problem...”
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    Article
  3. 123
    Effects of LOX Particle Diameter on Combustion Characteristics of a Gas-Liquid Pintle Rocket Engine
    by Xuan Jin, Chibing Shen, Rui Zhou, Xinxin Fang
    Published 2020-01-01
    “...LOX/GCH4 pintle injector is suitable for variable-thrust liquid rocket engines. In order to provide...”
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    Article
  4. 124
    Original Romanian Research for a Rocket Engine with Multiple Combustion Chambers during 1940 - 1944
    Subjects: “...rocket engine...”
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    Article
  5. 125
    Numerical study of the effect of the fuel film on heat transfer in a rocket engine combustion chamber
    by Goh, Sing Huat
    Published 2012
    “...-fueled rocket engine with an injected fuel film on the wall has been numerically simulated. The engine...”
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  6. 126
    Investigation of driving mechanisms of combustion instabilities in liquid rocket engines via the dynamic mode decomposition
    by Quinlan, John Mathew
    Published 2016
    “... modes can cause catastrophic failure in liquid rocket engines and to predict and prevent...”
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  7. 127
    A study on the spray characteristics of the gas centered swirl coaxial injector for liquid rocket engine
    by Tsung-LinYeh, 葉宗霖
    Published 2015
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  8. 128
    Experimental evaluation of hybrid propulsion rocket engine operating with paraffin fuel grain and gaseous oxygen
    by Genivaldo Pimenta dos Santos
    Published 2014
    “.... In this work combustion instability presented by rocket engine was calculated applying the frequency...”
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  9. 129
    Analysis of a heavy lift launch vehicle design using small liquid rocket engines
    by Russ, David Phillip
    Published 2007
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  10. 130
    Low-thrust liquid-propellant rocket engines as part of advanced ultralight rocket vehicle systems
    Subjects: “...rocket engine...”
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    Article
  11. 131
    The effect of departure from ideality of a multiply ionized monatomic gas on the performance of rocket engines
    by Perkins, John Noble
    Published 2014
    Subjects: “...Rocket engines -- Fuel systems...”
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  12. 132
    Dataset of the experimentally measured heat transfer in the throat region of liquid rocket engine thrust chambers
    by Marco Pizzarelli
    Published 2021-08-01
    Subjects: “...Liquid rocket engines...”
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    Article
  13. 133
    Design, Production and Evaluation of 3D-Printed Mold Geometries for a Hybrid Rocket Engine
    Subjects: “...hybrid rocket engine...”
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    Article
  14. 134
    Analysis of Chinese Cryogenic Long March Launch Vehicles and YF-100 Liquid Rocket Engine
    by Gordon, Kayleigh Elizabeth
    Published 2018
    Subjects: “...liquid rocket engine...”
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  15. 135
    Analysis of Nuclear Thermal Rocket Engine Coolant Channel Designs Enabled byAdditive Manufacturing
    by Salamon, Nicholas C.
    Published 2020
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  16. 136
    An anthology of outstanding achievements in science and technology. Part 18: Rocket engineering and near-space exploration
    by M.I. Baranov
    Published 2014-03-01
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    Article
  17. 137
    Development and analysis of simulation of liquid-propellant rocket engine pump head curve obtaining process
    by D. A. Savchin, V. P. Nazarov
    Published 2021-03-01
    “... in consideration of the implementation of automated systems in liquid-propellant rocket engine manufacturing...”
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    Article
  18. 138
    A Concept for Striking Range Improvement of the GROM/PIORUN Man-Portable Air-Defence System
    Subjects: “...rocket engine...”
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    Article
  19. 139
    The issue of ensuring the safe explosion of the spent orbital stages of a launch vehicle with propulsion rocket engine
    “... (SLV) with a propulsion rocket engine (PRE) based on the gasification of unusable residues propellant...”
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    Article
  20. 140
    A Reduced Order Model based on Large Eddy Simulation of Turbulent Combustion in the Hybrid Rocket Engine
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    Article
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