Conceptual design of single-stage launch vehicle with hybrid rocket engine using design informatics
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]
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
Handbook of Recommended Practices for the Determination of Liquid Monopropellant Rocket Engine Performance, [PDF]
R. A. Bjorklund+2 more
openalex +1 more source
PARALLEL UNSTEADY TURBOPUMP SIMULATIONS FOR LIQUID ROCKET ENGINES [PDF]
Cetin C. Kiris, Dochan Kwak, W. Chan
openalex +1 more source
The prediction of the nonlinear behavior of unstable liquid rockets [PDF]
Analytical technique for solving nonlinear combustion problems associated with liquid propellant rocket ...
Powell, E. A., Zinn, B. T.
core +1 more source
On possibility to use flow control units of electromagnetic type for liquid propellant rocket engines [PDF]
С. А. Шевченко
openalex +1 more source
Novel propellant settling strategies for liquid rocket engine restart in microgravity
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]
Shear layer mixing, hydrocarbon oxidation, and carbon cloud radiation models for liquid rocket engine exhaust plume ...
Edelman, R., Fortune, O.
core +1 more source
A Numerical Study on Sensitivity of Acoustic Response to Pressure Oscillations in Liquid Rocket Engine [PDF]
Chae-Hoon Sohn
openalex +1 more source
Summary of literature survey of hypergolic ignition spike phenomena, phase I Final report, Apr. 8 - Dec. 31, 1965 [PDF]
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