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Shear coaxial injector spray combustion experiments in a single element rocket chamber
A. Maskrey
, C. Puissant
, M. Glogowski
, M. M. Micci
Aerospace Engineering
Materials Research Institute (MRI)
Research output
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Contribution to conference
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Paper
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peer-review
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Keyphrases
Rocket
100%
Single Element
100%
Chamber Pressure
100%
Shear Coaxial Injector
100%
Combustion Experiment
100%
Spray Combustion
100%
Injector
50%
Acoustics
50%
Combustion
50%
Full-size
50%
Acoustic Pressure
50%
Vaporization Process
50%
Acoustic Response
50%
Liquid Oxygen
50%
Gaseous Hydrogen
50%
Combustion Chamber
50%
Plenum
50%
Mixture Ratio
50%
Pressure Oscillation
50%
Fuel Blends
50%
Engineering
Flow Rate
100%
Single Element
100%
Chamber Pressure
100%
Spray Combustion
100%
Flow Velocity
100%
Full Scale
50%
Acoustic Pressure
50%
Vaporization
50%
Element Model
50%
Combustion Chamber
50%
Liquid Oxygen
50%
Earth and Planetary Sciences
Flow Velocity
100%
Pressure Chamber
100%
Vaporization
50%
Pressure Oscillation
50%
Combustion Chamber
50%
Liquid Oxygen
50%