Experimental research on key technologies for future launcher propulsion

Keyphrases

• Propulsion 100%
• Thrust Chamber 100%
• Launcher 100%
• Heat Sink 66%
• Combustion Chamber 33%
• Injector 33%
• Gas Generator 33%
• Hot Gas 33%
• Mixture Ratio 33%
• Space Transportation 33%
• Operating Conditions 33%
• Material Sample 33%
• Single Element 33%
• Pressure Ratio 33%
• Heat Transfer 33%
• Element Design 33%
• Staged Combustion 33%
• Heat Release 33%
• Combustion Efficiency 33%
• Water Cooling 33%
• Scale Levels 33%
• Kerosene 33%
• Gaseous Oxygen 33%
• Hot Fire Test 33%
• Engine Design 33%
• Oxidation Resistance 33%
• Qualification Test 33%
• Spray Diagnostics 33%
• Past-present 33%

Engineering

• Critical Micelle Concentration 100%
• Hot Gas 50%
• Early Stage 50%
• Design Element 50%
• Development Process 50%
• Single Element 50%
• Key Parameter 50%
• Operational Condition 50%
• Heat Release 50%
• Test Material 50%
• Main Stage 50%
• Material Sample 50%
• Scale Level 50%
• Oxidation Resistance 50%
• Test Bench 50%
• Test Facility 50%
• Engine Design 50%
• Combustion Chamber 50%
• Gas Generator 50%