Results 171 to 180 of about 25,713 (266)
Pair propellants analysis for liquid rocket engine using the energetic and mass comparison
, 2013 Fábio Rezende Prado dos Santos
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Cryogenic propellant management in space: open challenges and perspectives. [PDF]
NPJ MicrogravitySimonini A +9 more
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Nonlinear combustion instability in liquid-propellant rocket motors
, 1968 S. Z. Burstein, W. Chinitz
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Development of a Liquid-Propellant Rocket Powered by a Rotating Detonation Engine
Journal of Propulsion and Power, 2023This paper presents work on a demonstrator rocket powered by a rotating detonation engine (RDE) fed by liquid propellants. Key to the success of the project was the development of a suitably efficient and lightweight RDE. After selecting the propellants:
M. Kawalec +3 more
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Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2022
The main objective of this study is to investigate the effect of turbine inlet temperature on the transient phase of expansion cycle liquid propellant rocket engines during start.
Mehrad Amin Eskandari +3 more
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The main objective of this study is to investigate the effect of turbine inlet temperature on the transient phase of expansion cycle liquid propellant rocket engines during start.
Mehrad Amin Eskandari +3 more
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Fundamental Concepts of Liquid-Propellant Rocket Engines
2021Alessandro de Iaco Veris
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History of liquid propellant rocket engines
Choice Reviews Online, 2006Leonie Kohl
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Liquid Propellant Rocket Motors
The Journal of the Royal Aeronautical Society, 1953It has been said that a rocket motor is the simplest “ prime mover.” This is correct in theory, since fundamentally a rocket consists of a chamber containing a gas under pressure, having a nozzle at one end through which the gas expands, forming a propulsive jet. Since the pressure ratio of the rocket is always greater than the critical pressure ratio,
B. R. Diplock +2 more
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Electric Feed Systems for Liquid-Propellant Rockets
Journal of Propulsion and Power, 2013Liquid-propellant rocket feed systems based on electric pumps are compared with the more classical pressure–gas and turbopump systems. The design parameters entering in the definition of the system mass are highlighted, and a careful choice of the figures of merit is performed, in particular for the electric motors and batteries.
P. A. Pavlov Rachov +2 more
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