Study of Different Al/Mg Powders in Hydroreactive Fuel Propellant Used for Water Ramjet

Engineering

• Burning Rate 100%
• Combustion Stage 100%
• Al Powder 100%
• Ray Diffraction 50%
• Good Performance 50%
• Combustor 50%
• X-Ray Diffraction Pattern 50%
• Onset Temperature 50%
• Propellant System 50%

Material Science

• Aluminum Alloys 100%
• Magnesium Powder 100%
• Magnesium 83%
• Powder 66%
• Aluminum-Magnesium Alloys 50%
• Thermogravimetric Analysis 33%
• X-Ray Diffraction 33%
• Oxidation Reaction 16%
• Scanning Electron Microscopy 16%
• Diffraction Pattern 16%