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Liquid-Propellant Rocket Engines
2012The liquid-propellant rocket engine has the characteristics that allow it to deliver thrust at a high-performance level, with an efficiency and operational flexibility that enables a number of mission applications to go forward. Monopropellant and bipropellant versions of this category of engine are discussed in some detail in this chapter.
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Modeling and robust analysis of a liquid rocket engine [PDF]
36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2000 Stability and dynamic performance of liquid-propellant rocket engines (LPRE) are two of the fundamental issues in the enginevehicle integration process. This analysis requires the construction of a detailed model, trying to capture the most realistic phenomena involved, which generally include several sources of uncertainties.
A. Santana +3 more
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Summarization on variable liquid thrust rocket engines
Science in China Series E: Technological Sciences, 2009The technology actuality and development trend of variable thrust rocket engines at home and abroad are summarized. Key technologies of developing variable thrust rocket engines are analyzed. Development advices on developing variable thrust rocket engines that are adapted to the situation of our country are brought forward.
XiPing Feng +4 more
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Interaction of Combustion with Transverse Velocity Fluctuations in Liquid Rocket Engines
, 2015The verification of thermoacoustic stability is one of the most essential steps in the framework of the development of liquid rocket engines. In hybrid methods, which allow fast and detailed evaluation of the flame/acoustics interaction, the simulation ...
T. Sattelmayer, M. Schmid, M. Schulze
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Fundamental Concepts of Liquid-Propellant Rocket Engines
2020The engine of a rocket vehicle is a machine which produces thrust by accelerating a gas flowing through the machine. The reaction to this acceleration is the force which drives the vehicle. The amount of thrust generated depends on the mass flow rate of the gas moving through the engine and on the exit velocity of the gas from the nozzle. The gas flow,
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Metal-matrix composites for liquid rocket engines
JOM, 2001This article presents an overview of current research and material requirements for metal-matrix composite (MMC) technologies being developed for liquid rocket engines (LRE). Developments in LRE technology for the U.S. Air Force are being tracked and planned through the integrated high payoff rocket propulsion technologies program (IHPRPT).
J. S. Shelley, J. Nichols, R. LeClaire
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Chemical modeling for methane oxy-combustion in Liquid Rocket Engines
Acta Astronautica, 2022Simon Blanchard, Q. Cazères, B. Cuenot
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Liquid-Propellant Rocket Engine Injector Dynamics
Journal of Propulsion and Power, 1998The dynamic characteristics of liquid-rocket injectors in the presence of intense combustion-chamber and propellant feed-line oscillations are discussed. Liquid-propellant injectors always function in nonsteady e ow environments and are therefore considered as a dynamic component of an engine.
Vladimir G. Bazarov, Vigor Yang
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History of the Titan liquid rocket engines [PDF]
25th Joint Propulsion Conference, 1989 L. Meland, F. Thompson
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