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EPATS Conference ILA Berlin, May 28, 2008. Missions Requirement for EPATS Aircraft. Affordable Personal Air Transport. WP4 Leader: Institute of Aviation / Włodzimierz Gnarowski Presentation: Institute of Aviation / Micha ł Pokorski. EPATS Conference ILA Berlin, May 28, 2008.
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EPATS Conference ILA Berlin, May 28, 2008 Missions Requirement for EPATS Aircraft Affordable Personal Air Transport WP4 Leader: Institute of Aviation / Włodzimierz Gnarowski Presentation: Institute of Aviation / Michał Pokorski
EPATS Conference ILA Berlin, May 28, 2008 REQUIREMENTS STRUCTURE 80% runways available • Airport performances • Mission requirements • - Range • - Flight levels • - Cruise speed • Operating • - Life Time • Regulations - CS-23 Range limits to needs The most favourable flight conditions
EPATS Conference ILA Berlin, May 28, 2008 REFERENCE AIRCRAFT SELECTION
EPATS Conference ILA Berlin, May 28, 2008 FUTURE AIRCRAFT DESIGN: 2020 RzUoT CESAR results NLR IoA Analyses DESIGN PROCESS SESAR requirements PZL-M PZL-Rz
EPATS Conference ILA Berlin, May 28, 2008 AIRCRAFT DESIGN PROCESS This is not a full conceptual design
EPATS Conference ILA Berlin, May 28, 2008 AIRCRAFT COMPARISION: Reference vs Future PISTONS 1eng 4seat 2eng 6seat TURBO-PROPS 2eng 8pax 2eng 19pax JETS 2eng 8pax 2020 short (long) distance
EPATS Conference ILA Berlin, May 28, 2008 FUTURE AIRCRAFT PERFORMANCE: 2020 Pistons T-PropsJets 8pax: T-Prop vs Jet Speed: -8 (-19)% DOC: -28 (-19)% SFC: -39 (-34)% Airplanes’ features as a functions of distance
EPATS Conference ILA Berlin, May 28, 2008 REMARKS - OPERATING Distance Impact DOC Very Sensitive to Utilization Intensity Today Indirect Cost level: 100 % DOC Future goal: 50 % DOC
EPATS Conference ILA Berlin, May 28, 2008 REMARKS – AIRSPACE STRUCTURE PROPOSAL Economic Parameters Current Airspace Load Fuel Consumption Different airplanes – different performances – different favourable flight conditions
EPATS Conference ILA Berlin, May 28, 2008 CONCLUSIONS • Affordable personal air transport is REAL. • Aircraft fitted to needs: • Range, speed, size, etc. • Operating optimization: • High utilization intensity, • Low indirect cost. • Pistons and turbo-props the most suitable.
EPATS Conference ILA Berlin, May 28, 2008 Thank you for your attention