Chi-Ming Lee Chief of Combustion Branch NASA Glenn Research ...

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Fischer-Tropsch & Jet A Fuel Analysis Test F-T Jet A Total Acid Number (mg KOH/g) 0.002 0.00 Aromatics (% vol) 0.0 19 Mercaptan Sulfur (% mass) 0.000 0.000 Total Sulfur (% mass) 0.00 0.0 Distillation Initial Boiling Point (°C) 149 10% Recovered (°C) 162 180 20% Recovered (°C) 163 50% Recovered (°C) 168 212 90% Recovered (°C) 184 251 End Point (°C) 196 Residue (% vol) 0.9 1.3 Loss (% vol) 0.4 0.9 Flash Point (°C) 44 51 API Gravity @ 60°F 60.5 Freezing Point (°C) -55 -48 Viscosity @ -20°C (mm²/s) 2.6 5.2 Net Heat <strong>of</strong> <strong>Combustion</strong> (MJ/kg) 44.2 Test F-T Jet A Hydrogen Content (% mass) 15.6 Smoke Point (mm) 40.0 21 Copper Strip Corrosion (2 h @ 100°C) 1a Thermal Stability @ 260°C Change in Pressure (mmHg) Tube Deposit Rating, Visual Existent Gum (mg/100 mL)
Time--> C 8 C 9 C 10 C 11 F-T Fuel Analysis C 12 5 10 15 20 25 30 C 13 C 14 C 15 5172 F-T Kerosene C 16 Syntroleum 4909 S-8 C 17 C 18 C 19 11
Page 1 and 2: Chi-Ming Lee Chief of Combustion Br
Page 3 and 4: NOx emissions vs. the Overall Press
Page 5 and 6: Flametube Combustor Emissions Reduc
Page 7 and 8: Fuel Flexible/Low Emissions Combust
Page 9: 75% Nox Reduction Injector Developm
Page 13 and 14: JP8, 50-50 Blend, and FT-2 Comparis
Page 15 and 16: ASCR Plenum Design and Fabrication
Page 17 and 18: Ultra-Lean-Burning Combustors Are M
Page 19 and 20: Long Term Goal for Active Combustio
Page 21 and 22: Active Combustion Control Combustio
Page 23 and 24: SiC Electronics Status • Building
Page 25 and 26: SiC Pressure Sensor Status • The
Page 27 and 28: High Temperature Combustor Liner Ch
Page 29 and 30: ERA CMC LINER - Subtasks 1. Liner m
Page 31 and 32: ERA CMC Liner Material Testing- Env
Page 33 and 34: High Temperature Piezoelectric Mate

Chi-Ming Lee Chief of Combustion Branch NASA Glenn Research ...

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