Effects of LOX Particle Diameter on Combustion Characteristics of a Gas-Liquid Pintle Rocket Engine
, 2020 LOX/GCH4 pintle injector is suitable for variable-thrust liquid rocket engines. In order to provide a reference for the later design and experiments, three-dimensional numerical simulations with the Euler-Lagrange method were performed to study the ...
Xu Jin +3 more
semanticscholar +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. +2 more
core +1 more source
Dataset of the experimentally measured heat transfer in the throat region of liquid rocket engine thrust chambers. [PDF]
Data Brief, 2021 Pizzarelli M.
europepmc +1 more source
Combustion instability research Summary report, 1970 [PDF]
Combustion instability in liquid rocket ...
Bracco, F. V. +9 more
core +1 more source
Design and testing of liquid hydrogen-cooled, ultrahigh-speed ball bearings [PDF]
, 1969 Large-bore, liquid hydrogen-cooled, ultrahigh-speed, rolling contact bearings of an optimum design allow optimization of large rocket engine turbopumps in which bearing speed is a limiting factor.
Butner, M. F., Wagner, D. A.
core +1 more source
Investigation of the cooling film distribution in liquid rocket engine [PDF]
Journal of Aerospace Technology and Management, 2011 This study presents the results of the investigation of a cooling method widely used in the combustion chambers, which is called cooling film, and it is applied to a liquid rocket engine that uses as propellants liquid oxygen and kerosene.
Luís Antonio Silva
doaj
Diversity of design knowledge for launch vehicle in view of fuels on hybrid rocket engine
Journal of Advanced Mechanical Design, Systems, and Manufacturing, 2014 A single-stage launch vehicle with hybrid rocket engine, which uses solid fuel and liquid oxidizer, has been studied and developed as a next-generation rocket for scientific observation due to the advantages as low cost, safety, re-ignition, and reduced ...
Kazuhisa CHIBA +4 more
doaj +1 more source
Electrodynamic actuators for rocket engine valves [PDF]
, 1972 Actuators, employed in acoustic loudspeakers, operate liquid rocket engine valves by replacing light paper cones with flexible metal diaphragms. Comparative analysis indicates better response time than solenoid actuators, and improved service life and ...
Doshi, D., Fiet, O.
core +1 more source
, 2017 NASA and industry partners are working towards fabrication process development to reduce costs and schedules associated with manufacturing liquid rocket engine components with the goal of reducing overall mission costs. One such technique being evaluated
P. Gradl +5 more
semanticscholar +1 more source
Nonlinear Aspects of Combustion Instability in Liquid Propellant Rocket Motors. Second Yearly Progress Report for the Period 1 June 1961 to 31 May 1962 [PDF]
Combustion instability in liquid-propellant rocket ...
Harrje, D. T. +2 more
core +1 more source