1. The Greenliner Environmentally Friendly Aircraft Tom Berger AA241B 3/14/06

2. Why Environmentally Friendly? Increasing Demand for Aviation  Growing Impact on Environment Regulations: ACARE Report “European Aeronautics – a Vision for 2020” –Reduce fuel consumption and CO 2 emissions by 50% –To reduce NO X emissions by 80% –Reduce perceived external noise by 50 per cent. Current Aircraft in Production –Boeing 787, Airbus A350

3. Baseline - Design

4. Baseline - Requirements BaselineRequirements Range5411 nmi6000 nmi Climb0.00380.024 TO Field5520 ft7500 ft Landing Field3271 ft5000 ft D/T0.688<0.88

5. Baseline – Summary Chart

6. Modifications MTOW: –447310  379240 lbs Sref: –4000  2987.8 ft 2 Thrust per engine –66138  59204 lbs Wing AR –9.5  11 S h /S ref –0.175  0.2667

7. Final Design

8. Final Design - Requirements Final DesignRequirements Range6000 nmi Climb0.024 TO Field7000 ft7500 ft Landing Field4000 ft5000 ft D/T0.602<0.88

9. Final Design - Specifications MTOW (lbs) 379,239Wing X/L0.28 Sref (ft 2 )2987.8Wing AR11 Thrust (lb)118,408 Cruise Mach 0.78 Init Alt (ft)32,000Est Fare$689.52 Final Alt (ft) 39,000Price$68.5

10. Final Design - Summary

11. Emissions 767* Greenliner ChangeDesired CO 2 (kg/pax- km)** 0.1670.057-65.9%-50% *** H 2 O (kg/pax-km)** 0.0650.0348-46.5% NO x (g/pax-km)** 0.7570.631-16.6%-80% *** NO X Exceed (kg) -9.94 (-28%) Noise (dB) -11.0-10 * Source: SAS Emission Calculator ** 65% Average Cabin Factor *** ACARE

12. Future Work Short Term –Cruise Altitude –Drag Long Term –Engine Design –Aircraft Design