Results 141 to 150 of about 67,829 (315)

Application of the substructure method for thermal stress-strain assessment of a liquid-propellant rocket engine combustion chamber [PDF]

open access: bronze, 2013
С.С. Гаврюшин   +4 more
openalex   +1 more source

Review of Combustion Stability Characteristics of Swirl Coaxial Element Injectors [PDF]

open access: yes
Liquid propellant rocket engine injectors using coaxial elements where the center liquid is swirled have become more common in the United States over the past several decades, although primarily for technology or advanced development programs. Currently,
Casiano, M. J., Hulka, J. R.
core   +1 more source

Liquid rocket engine axial-flow turbopumps [PDF]

open access: yes
The axial pump is considered in terms of the total turbopump assembly. Stage hydrodynamic design, pump rotor assembly, pump materials for liquid hydrogen applications, and safety factors as utilized in state of the art pumps are among the topics ...
Farquhar, J.   +4 more
core   +1 more source

Estimating model parameters of liquid rocket engine simulator using data assimilation

open access: yesActa Astronautica, 2020
Dai Satoh   +4 more
semanticscholar   +1 more source

Method for Determining Optimum Injector Inlet Geometry [PDF]

open access: yes
A method for determining the optimum inlet geometry of a liquid rocket engine swirl injector includes obtaining a throttleable level phase value, volume flow rate, chamber pressure, liquid propellant density, inlet injector pressure, desired target spray
Myers, W. Neill, Trinh, Huu P.
core   +1 more source

JANNAF "Test and Evaluation Guidelines for Liquid Rocket Engines": Status and Application [PDF]

open access: yes
For many decades, the U.S. rocket propulsion industrial base has performed remarkably in developing complex liquid rocket engines that can propel critical payloads into service for the nation, as well as transport people and hardware for missions that ...
Parkinson, Douglas   +2 more
core   +1 more source

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