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Turbopumps for Liquid Rocket Engines
SAE Technical Paper Series, 1992<div class="htmlview paragraph">This technical paper discusses the evolution of turbopumps designed for U.S. rocket engines, starting with the Thor, Jupiter, and Atlas missiles, which were developed in the 1950s; the F-1 and J-2 engines, which were developed in the 1960s for the Saturn V vehicle to put man on the moon; and the Space Shuttle Main ...
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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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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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Liquid rocket engine test plan comparison
37th Joint Propulsion Conference and Exhibit, 2001Tests quantity, number of Engines fired, total cumulated firing time performed during development are key factors for reliability estimation, but above all, for Launcher customer trust. In other respect schedule and development cost are first order dependant of the Engine test plan: the difference between a high number of tests and a low rate test plan
Pascal Pempie, Hilda Vernin
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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 ROCKET ENGINE RELIABILITY CERTIFICATION
2017<div class="section abstract"> <div class="htmlview paragraph">Current design and development practices leading to formal liquid rocket engine qualification (USAF) or certification (NASA) will not achieve the specific reliability objectives of future programs.
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International Conference on Mechanical and Aerospace Engineering, 2018
A dynamic model of a liquid-propellant rocket engine has been developed in this paper, with the future purpose of meeting the more demanding requirements of rocket-engines control forced by the new reusability scenarios.
Sergio Pérez-Roca +6 more
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A dynamic model of a liquid-propellant rocket engine has been developed in this paper, with the future purpose of meeting the more demanding requirements of rocket-engines control forced by the new reusability scenarios.
Sergio Pérez-Roca +6 more
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Design of liquid-propellant rocket engines
Journal of Machinery Manufacture and Reliability, 2012A design method for liquid-propellant rocket engines is proposed, on the basis of models adjusted in response to test results. This method increases the reliability of the results and reduces ground testing of the motors. The effectiveness of the method is confirmed by ground testing and flight experience with the motors developed by Salyut Design ...
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Regenerative cooling for liquid rocket engines
Journal of Thermal Science, 1995Heat transfer in the thrust chamber is of great importance in the design of liquid propellant rocket engines. Regenerative cooling is an advanced method which can ensure not only the proper running but also higher performance of a rocket engine. The theoretical model is complicated, it relates to fluid dynamics, heat transfer, combustion, etc...
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