2005 / 1 / 5 Update.

Bell Aerosystems	Bell X-22A VTOL Experimental Aircraft Length : 12.06m Wing Span (Front) : 7.0m Wing Span (Rear) : 11.96m Hight : 6.31m Wing Area (Front) : 12.91 Square meter Wing Area (Rear) : 26.57 Square meter All-Up Weight : 8,172Kg Empty Weight : 5,197Kg Engine : General Electric YT58-GE-8D Turbo Shaft (1,050shp) X 4 Max Speed : 410Km/h Max Altitude : 8,500m Range : 720Km Crew : 2
Boeing	Boeing X-50 CRW (Canard Rotor Wing) Experimental Aircraft