Results 121 to 130 of about 39,486 (297)

Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines

open access: yesActa Astronautica, 2020
W. Armbruster   +4 more
semanticscholar   +1 more source

Extended temperature range rocket injector [PDF]

open access: yes, 1991
A rocket injector is provided with multiple sets of manifolds for supplying propellants to injector elements. Sensors transmit the temperatures of the propellants to a suitable controller which is operably connnected to valves between these manifolds and
Schneider, Steven J.
core   +1 more source

A compressible two-phase flow framework for Large Eddy Simulations of liquid-propellant rocket engines

open access: yesApplied Mathematical Modelling, 2020
C. L. Touze   +3 more
semanticscholar   +1 more source

Ablative response of a silica phenolic to simulated liquid propellant rocket engine operating conditions [PDF]

open access: yes
Ablative response of silica phenolic to simulated liquid propellant rocket engine operating ...
Moyer, C. B.   +3 more
core   +1 more source

Rocket engine injector Patent [PDF]

open access: yes, 1968
Rocket engine injector orifice to accommodate changes in density, velocity, and pressure, thereby maintaining constant mass flow rate of propellant into rocket combustion ...
Stein, S.
core   +1 more source

Dual-fuel, dual-mode rocket engine [PDF]

open access: yes, 1989
The invention relates to a dual fuel, dual mode rocket engine designed to improve the performance of earth-to-orbit vehicles. For any vehicle that operates from the earth's surface to earth orbit, it is advantageous to use two different fuels during its ...
Martin, James A.
core   +1 more source

A study of high frequency nonlinear combustion instability in baffled annular liquid propellant rocket motors, volume 1 Final report, 25 Aug. 1969 - 25 Sep. 1970 [PDF]

open access: yes
High frequency nonlinear combustion instability in baffled annular liquid propellant rocket engines - Vol.
Burstein, S. Z., Schechter, H. S.
core   +1 more source

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