The Pagotto Brakogyro is a series of Italianautogyros, designed by Enio Pagotto and produced by Carpenterie Pagotto of Pianzano. The aircraft is supplied as a complete ready-to-fly-aircraft.[1]
The aircraft fuselage is made from welded stainless steel tubing, with a non-structural composite cockpit fairing. Its 8.53 m (28.0 ft) diameter Averso rotor has a chord of 21.3 cm (8.4 in). The aircraft has a triple tail mounted on the tail boom tube.[1]
Variantsedit
Brakogyro GT
Model with composite cockpit fairing. The Brakogyro GT has an empty weight of 265 kg (584 lb) and a gross weight of 450 kg (992 lb), giving a useful load of 185 kg (408 lb).[1]
NAKEd
Open model without the cockpit fairing, but fitted with a single rollbar and skids in front of the main landing gear. The NAKEd has an empty weight of 248 kg (547 lb) and a gross weight of 450 kg (992 lb), giving a useful load of 202 kg (445 lb), 17 kg (37 lb) more than the Brakogyro GT.[1]
pagotto, brakogyro, series, italian, autogyros, designed, enio, pagotto, produced, carpenterie, pagotto, pianzano, aircraft, supplied, complete, ready, aircraft, brakogyro, during, landing, role, autogyro, national, origin, italy, manufacturer, carpenterie, pa. The Pagotto Brakogyro is a series of Italian autogyros designed by Enio Pagotto and produced by Carpenterie Pagotto of Pianzano The aircraft is supplied as a complete ready to fly aircraft 1 Brakogyro Pagotto Brakogyro GT during landing Role Autogyro National origin Italy Manufacturer Carpenterie Pagotto Designer Enio Pagotto Status In production 2013 Contents 1 Design and development 2 Variants 3 Specifications Brakogyro GT 4 References 5 External linksDesign and development editThe Brakogyro features a single main rotor an open cockpit with a windshield with two seats in tandem tricycle landing gear with wheel pants and a four cylinder air and liquid cooled four stroke dual ignition Rotax 912S engine with a custom designed turbocharger that produces 122 hp 91 kW mounted in pusher configuration The 115 hp 86 kW turbocharged Rotax 914 powerplant is also available but at higher cost 1 The aircraft fuselage is made from welded stainless steel tubing with a non structural composite cockpit fairing Its 8 53 m 28 0 ft diameter Averso rotor has a chord of 21 3 cm 8 4 in The aircraft has a triple tail mounted on the tail boom tube 1 Variants editBrakogyro GT Model with composite cockpit fairing The Brakogyro GT has an empty weight of 265 kg 584 lb and a gross weight of 450 kg 992 lb giving a useful load of 185 kg 408 lb 1 NAKEd Open model without the cockpit fairing but fitted with a single rollbar and skids in front of the main landing gear The NAKEd has an empty weight of 248 kg 547 lb and a gross weight of 450 kg 992 lb giving a useful load of 202 kg 445 lb 17 kg 37 lb more than the Brakogyro GT 1 Specifications Brakogyro GT editData from Bayerl 1 General characteristicsCrew one Capacity one passenger Empty weight 265 kg 584 lb Gross weight 450 kg 992 lb Fuel capacity 80 litres 18 imp gal 21 US gal Powerplant 1 Rotax 912ULS Turbo four cylinder liquid and air cooled four stroke aircraft engine fitted with a Pagotto designed turbocharger 91 kW 122 hp Main rotor diameter 8 53 m 28 ft 0 in Propellers 3 bladed compostire Performance Maximum speed 195 km h 121 mph 105 kn Cruise speed 150 km h 93 mph 81 kn Rate of climb 5 m s 980 ft min References edit a b c d e f Bayerl Robby Martin Berkemeier et al World Directory of Leisure Aviation 2011 12 page 185 WDLA UK Lancaster UK 2011 ISSN 1368 485XExternal links edit nbsp Wikimedia Commons has media related to Pagotto Brakogyro Official website Portals nbsp Italy nbsp Companies nbsp Aviation Retrieved from https en wikipedia org w index php title Pagotto Brakogyro amp oldid 1126664839, wikipedia, wiki, book, books, library,
