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Combustion of boron and fluorocarbon solid fuels in a hybrid rocket
Terrence L. Connell
,
Grant A. Risha
,
Richard A. Yetter
, Colin W. Roberts
, Gregory Young
Division of Business, Engineering, and Information Sciences & Technology (Altoona)
Mechanical Engineering
Research output
:
Chapter in Book/Report/Conference proceeding
›
Conference contribution
2
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Scopus citations
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Keyphrases
Deflagration
100%
Fluorocarbon
100%
Solid Fuel
100%
Hybrid Rocket
100%
Oxidizer
75%
Constant Pressure
75%
Pressure Dependence
75%
Low Pressure
50%
Burning Rate
50%
Fuel Blends
50%
Boron
25%
Operating Conditions
25%
Oxygen Content
25%
Polytetrafluoroethylene
25%
Performance Parameters
25%
The Self
25%
Combustion Efficiency
25%
Strong Dependence
25%
Pressurization Rate
25%
Strand Burner
25%
Pressure Range
25%
Regression Rate
25%
Nozzle Throat
25%
Nitrogen Environment
25%
Composite Propellant
25%
Fuel Regression Rate
25%
Rocket Motor
25%
Heat Mass Transfer
25%
Flow Dependency
25%
Pure Oxygen
25%
Additional Resistance
25%
Fluorination
25%
Rate Correlation
25%
Oxygen Mass Fraction
25%
Counterflow Burner
25%
Throat Area
25%
Exhaust Velocity
25%
Engineering
Solid Fuel
100%
Deflagration
100%
Oxidizer
75%
Dilution
50%
Burning Rate
50%
Flow Rate
25%
Strand
25%
Rocket Engine
25%
Performance Parameter
25%
Pressurization
25%
Conducted Experiment
25%
Ignition
25%
Oxygen Content
25%
Pressure Range
25%
Mass Fraction
25%
Char Surface
25%
Phase Composition
25%
Flow Velocity
25%
Pure Oxygen
25%
Throat Area
25%
Exhaust Velocity
25%
Material Science
Boron
100%
Dilution
100%
Density
50%
Composite Propellant
50%
Surface (Surface Science)
50%
Phase Composition
50%
Chemical Engineering
Deflagration
100%
Fluorocarbon
100%
Polytetrafluoroethylene
25%