Quality control automated laser-ultrasonic method for solder joints of nozzles of chambers in liquid rocket engines [PDF]
D. S. Sergeev+3 more
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Influence of extruded injector nozzle on fuel mixing and mass diffusion of multi fuel jets in the supersonic cross flow: computational study. [PDF]
Abdollahi SA+2 more
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Combustion chamber Patent [PDF]
Regenerative cooling system for rocket combustion chamber using coolant tubes in convergent-divergent ...
Gregory, J. W.
core +1 more source
Based on Fluent Numerical Calculation of Refractive Index on Rocket Engine Nozzle Plume
Qiangfeng Huang+5 more
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Scaling laws of plume-induced granular cratering. [PDF]
Gorman MT+6 more
europepmc +1 more source
Influence of Adding Carbonaceous Fuels to Ionic Liquids on Propellant Properties. [PDF]
Gao X, Gao Z, Tan Y, Chen P, Du Z, Li Y.
europepmc +1 more source
A Numerical Study on Carbon-Fiber-Reinforced Composite Cylindrical Skirts for Solid Propeller Rockets. [PDF]
Baldieri F, Martelli E, Riccio A.
europepmc +1 more source
Study on Rheological Properties and Pouring Process of Hydroxyl-Terminated Polybutadiene (HTPB) Propellants. [PDF]
Wang H, Ji Y, Jiang X, Li Z.
europepmc +1 more source
Improved stability analysis of rocket engine nozzles
This master’s thesis was conducted at Volvo Aero Corporation (VAC) in Trollhättan at the department of combustion chambers and nozzles. This department is responsible for the development of the main engine nozzle extension to the European Ariane 5 rocket. During space flight there are a variety of loads which may cause structural instability
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CONTOUR DESIGN FOR SOLID-PROPELLANT ROCKET-ENGINE NOZZLE
Minh Phu Nguyen
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