Transient Burning Characteristics of JA2 Propellant Using Experimentally Determined Zel'dovich Map

Authors :: Kenneth K. Kuo
Baoqi Zhang
Source :: Journal of Propulsion and Power. 22:455-461
Publication Year :: 2006
Publisher :: American Institute of Aeronautics and Astronautics (AIAA), 2006.
Abstract: Combustion characteristics of JA2 propellant were studied both experimentally and theoretically. Its steady-state burning behavior was investigated using an optical strand burner. The parameters measured were the regression rate, subsurface temperature profile, and burning surface temperature at different initial temperatures (-40

Subjects :: Propellant
Materials science
Temperature sensitivity
Mechanical Engineering
Aerospace Engineering
Thermodynamics
Regression rate
Combustion
Linear function
Fuel Technology
Space and Planetary Science
Combustor
Transient (oscillation)
Simulation

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