Results 91 to 100 of about 39,486 (297)

Simple Learning-Based Robust Nonlinear Control of an Electric Pump for Liquid-Propellant Rocket Engines [PDF]

, 2023
Mohammad Jafari, Mahmut Reyhanoglu, Zhandos Kozhabek   +2 more
openalex   +1 more source

Statistical derivation of design criteria for liquid rocket combustion instability Final report [PDF]

Statistical correlation between engine design and combustion stability in liquid propellant rocket ...
Bastress, E. K., Harris, G. H., Miller, I.   +2 more
core   +1 more source

Theoretical investigation on transverse mode combustion instability for liquid propellant rockets [PDF]

Mathematical solution of nonlinear transverse combustion instability problems in thin annular liquid propellant rocket ...
Crocco, L., Lorenzetto, J. H.
core   +1 more source

Nondestructive testing of brazed rocket engine components [PDF]

, 1968
Report details study made of nondestructive radiographic, ultrasonic, thermographic, and leak test methods used to inspect and evaluate the quality of the various brazed joints in liquid-propellant rocket engine components and assemblies. Descriptions of
Adams, C. J., Hagemaier, D. J., Meyer, J. A.   +2 more
core   +1 more source

On possibility to use flow control units of electromagnetic type for liquid propellant rocket engines [PDF]

, 2001
С. А. Шевченко
openalex   +1 more source

Steady state aerothermochemistry for liquid bipropellant rocket motors [PDF]

Model and theoretical equations describing liquid propellant droplet ballistics and combustion gas behavior in bipropellant rocket motors ...
Agosta, V. D., Burstein, S. Z.
core   +1 more source

Cold solid propellant motor has stop-restart capability [PDF]

, 1966
Solid propellant rocket is kept and fired at low temperatures in launch vehicles or spacecraft. The motor is capable of developing a specific impulse comparable to that of liquid propellant motors, is started, stopped, and restarted, and is stored in ...
Hendel, F. J.
core   +1 more source

PECULIARITIES OF COOLING COMBUSTION CHAMBER OF ROCKET ENGINE, WHICH UTILIZE HIGH-TEST PEROXIDE AS AN OXIDIZER

Авіаційно-космічна техніка та технологія, 2017
Interest in storable ecologically friendly propellant has increased recently. One of the reasons for that is convenience in storage, handle and delivery. The most interesting storable propellant for launch vehicles is high-test peroxide with kerosene.  A
Михаил Витальевич Андриевский, Юрий Алексеевич Митиков, Дмитрий Анатольевич Шамровский   +2 more
doaj   +1 more source

Radiative Heating in Combustion Chamber of Liquid Propellant Rocket Engines

, 2016
The effects of radiation heat transfer in rocket engine combustion chambers are studied analytically. The fuel is hydrogen, methane or ethanol, and the oxidizer is oxygen. Radiative heat fluxes are estimated using empirical equations, and convective heat
K. Takeshi, Satoshi Masaki
semanticscholar   +1 more source

EFFECT OF CONTACT ANGLE AND TANK GEOMETRY ON THE CONFIGURATION OF THE LIQUID-VAPOR INTERFACE DURING WEIGHTLESSNESS [PDF]

Effect of contact angle and space vehicle tank geometry on configuration of rocket propellant liquid-vapor interface during ...
Nussle, R. C., Otto, E. W., Petrash, D. A.   +2 more
core   +1 more source