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In 1932 the Air Ministry initiated a conversion of the Condor petrol engine to the compression ignition system. The conversion was developed at the Royal Aircraft Establishment, Farnborough, with the co-operation of Rolls-Royce Ltd. Engine layout, bore, and stroke remained the same as for the petrol version; the compression ratio increased to 12.5:1.
Transportation aircraft fitted with four BMW 132Dc engines; one built. Fw 200 B-2 Transportation aircraft fitted with four BMW 132H engines; three built. Fw 200 C-0 Pre-production batch of 10 aircraft, structural strengthening, the first four were manufactured as unarmed transports, the remaining six were fitted with armament. Fw 200 C-1
The Condor is powered by a 39.5 kW (53 hp) Rotax 503.2 V UL CB. The standard engine of the Condor Plus is the 48.5 kW (65 hp) Rotax 582 UL-DCDI , driving a two blade propeller, but the 59.7 kW (80 hp) Rotax 912 UL-DCDI or the 74.6 kW (100 hp) Rotax 912 ULS , both with three blade airscrews, are options.
The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg). The aircraft has a standard empty weight of 240 lb (109 kg). It features a cable-braced high-wing, open cockpit, tricycle landing gear and a single engine in pusher configuration.
Its two 635 hp (474 kW) Curtiss Conqueror pressurized water-cooled V-12 engines were mounted on top of the lower wing in long cowlings. Geared down from an engine optimum 2,400 rpm by a factor of two, they drove three-bladed propellers. They were cooled by longitudinally oriented, rectangular profile radiators proud above each cowling.
The Schweizer RU-38 Twin Condor is a two or three-seat, fixed gear, low wing, twin boom covert reconnaissance aircraft. [6] [7] RU-38 is the US military designation for the aircraft, indicating Utility, Reconnaissance. The Schweizer company model number is Schweizer SA 2-38A Condor and, in its three-seat configuration, Schweizer SA 3-38A Condor [8]
The Condor had a 141-hour flight test program and first flew on 9 October 1988, with two built. [3] In 1989, the Condor set the world piston-powered aircraft altitude record of 67,028 ft (20,430 m) and was the first aircraft to fly a fully automated flight from takeoff to landing.
Data from Jane's all the World's Aircraft 2006-07, Volga-Dnepr General characteristics Crew: Eight (pilot, copilot, navigator, chief flight engineer, electrical flight engineer, radio operator, two loadmasters) Capacity: 88 passengers in upper aft fuselage, or the hold can take an additional 350 pax on a palletised seating system / 150,000 kg (330,693 lb) Length: 69.1 m (226 ft 8 in) Wingspan ...