radome temperature:130°C (mach2,05) front cone auxiliary gear hatch main landing gear hatch leading flaps temperature 130C(mach2.05) flaps extemal flap rudder Figure 7.7 Composite Components in a Future Supersonic Aircraft Economically viable for a single type of aircraft on the market (enlarged international cooperation) 7.1.6 Regional Jets Example:Regional transport aircraft ATR 72,ATR (FRA-ITA)(Figure 7.8): ■Total mass:20tons Percentage of composite materials more than 25%of the mass of the structure ■ Transports 66 passengers over a distance of 2,600 kilometers Interior equipment:Facings of panels for portholes and ceiling,baggage compartment,bulkheads,toilets,storing armors in glass-carbon/phenolic resins/NOMEX honeycomb;decoration by a film of "TEDLAR" 2003 by CRC Press LLC
Economically viable for a single type of aircraft on the market (enlarged international cooperation) 7.1.6 Regional Jets Example: Regional transport aircraft ATR 72, ATR (FRA–ITA) (Figure 7.8):
Total mass: 20 tons
Percentage of composite materials more than 25% of the mass of the structure
Transports 66 passengers over a distance of 2,600 kilometers
Interior equipment: Facings of panels for portholes and ceiling, baggage compartment, bulkheads, toilets, storing armors in glass-carbon/phenolic resins/NOMEX honeycomb; decoration by a film of “TEDLAR” Figure 7.7 Composite Components in a Future Supersonic Aircraft TX846_Frame_C07 Page 144 Monday, November 18, 2002 12:17 PM © 2003 by CRC Press LLC