Results 91 to 100 of about 69,089 (320)

Conceptual design of single-stage launch vehicle with hybrid rocket engine using design informatics

open access: yesNihon Kikai Gakkai ronbunshu, 2014
A single-stage launch vehicle with hybrid rocket engine has been conceptually designed by using design informatics, which has three points of view, i.e., problem definition, optimization, and data mining.
Kazuhisa CHIBA   +4 more
doaj   +1 more source

Investigation of critical burning of fuel droplets [PDF]

open access: yes
Steady and unsteady combustion of liquid fuel droplets under rocket engine conditions was analyzed. Emphasis was placed on combustion at elevated pressures and temperatures.
Chanin, S., Faeth, G. M.
core   +1 more source

The prediction of the nonlinear behavior of unstable liquid rockets [PDF]

open access: yes
Analytical technique for solving nonlinear combustion problems associated with liquid propellant rocket ...
Powell, E. A., Zinn, B. T.
core   +1 more source

Novel propellant settling strategies for liquid rocket engine restart in microgravity

open access: yesActa Astronautica, 2022
Á. Romero-Calvo   +4 more
semanticscholar   +1 more source

The effect of mixing, radiation, and finite rate combustion upon the flow field and surroundings of the exhaust plumes of rocket engines burning RP1 /kerosene/ and liquid oxygen [PDF]

open access: yes
Shear layer mixing, hydrocarbon oxidation, and carbon cloud radiation models for liquid rocket engine exhaust plume ...
Edelman, R., Fortune, O.
core   +1 more source

Summary of literature survey of hypergolic ignition spike phenomena, phase I Final report, Apr. 8 - Dec. 31, 1965 [PDF]

open access: yes
Summary of industry survey and literature search of ignition spike phenomena in low thrust, hypergolic, liquid bipropellant rocket ...
Christos, T., Perlee, H. E.
core   +1 more source

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