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Combustion studies of boron, magnesium, and aluminum composite propellants
A. Ishihara,
M. Q. Brewster
Mechanical Science and Engineering
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peer-review
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Keyphrases
Condensed Phase
100%
Combustion
100%
Boron
100%
Aluminum Composite
100%
Composite Propellant
100%
Magnesium Matrix Composites
100%
Magnesium
60%
Heat Release
60%
Burning Rate
60%
Aluminized Propellant
60%
Ammonium Perchlorate
40%
Heat Feedback
40%
Radiative Feedbacks
40%
Propellant Burning Rate
40%
Thermocouple
20%
Oxides
20%
Optical Fiber
20%
Sensitivity Analysis
20%
Feedback Cycle
20%
Heat Conductivity
20%
Propellant
20%
Radiative Heat
20%
Combustion Behavior
20%
Hydroxyl-terminated Polybutadiene Propellant
20%
Material Science
Boron
100%
Magnesium
100%
Aluminum Composite
100%
Composite Propellant
100%
Surface (Surface Science)
50%
Fiber Optics
25%
Oxide Compound
25%
Aluminum
25%
Polybutadiene
25%
Engineering
Burning Rate
100%
Heat Release
60%
Conductive
20%
Fiber Optics
20%
Relative Importance
20%
Thermocouple
20%
Chemical Engineering
Polybutadiene
100%
Earth and Planetary Sciences
Polybutadiene
20%