Kordin 1911 monoplane
Kordin 1911 monoplane
Engines – Power
Koppen Skyfarer
Otto Koppen left Ford to join the faculty of MIT, and in 1938, he decided that the time was ripe for an easy to fly airplane, so while teaching at MIT, he designed and set up a company to produce the Skyfarer, a two seat, two control monoplane. Koppen felt the Skyfarer needed no rudder, since its large twin vertical stabilizers were widely spaced on the tail out of the slipstream. In the air, the ball stayed centered at all times. In fact, the Skyfarer was so easy to fly that a complete novice was once taught the basics during only 50 minutes in the airplane. Twenty five Skyfarers were built; then World War II began, the Government requisitioned aluminum and production stopped.
Kopcsa 1913 Monogyroplane
In 1913 Romanian émigré Alexander Kopcsa (often found written as Kopesa and Kopsca, his original Romanian name was Alexandru Copcea), living in Chicago, invented this large flying machine (span 50 feet and length 40 feet), intended to be used in an attempt to fly across the Atlantic Ocean. The 170 hp engine was to turn two vertical and two horizontal propellers.
Koolhoven F.K.59
The type number F.K.59 has been used for three Koolhoven designs: a two-engined float plane, an open two-seat sports plane and a single engined military biplane developed from the F.K.52. Of these three aircraft it was the single engined biplane that made it to production as Koolhoven F.K.59, first flown in 1940. It was the last Koolhoven design in production.
Other sources mostly show a photo of the two-engined float plane as F.K.59, but this was just a mock-up, not an actual aircraft, neither a prototype.
Koolhoven FK.58
Dutch single seat fighter aircraft. The NV Koolhoven Vliegtuigen of Waalhaven, near Rotterdam, built the prototype F.K.58 within two months of completion of the design, and it flew for the first time on July 17, 1938, bearing the civil registration PH ATO. Designed by Dr Erich Schatzki, formerly of Fokker, to meet a French requirement, the F.K.58 had plywood covered wooden wings and fixed tail surfaces; a metal and fabric-covered steel tube fuselage; and metal framed fabric covered wing and tail control surfaces. A total of 450 litres (99 Imperial gallons) of fuel was carried internally, and the 1080 hp Hispano Suiza 14Aa 14 cylinder two row radial engine gave it a top speed of 483 km/h (300 mph).
This prototype was demonstrated to the French authorities at the Centre d’Essais du Materiel Aeden at Villacoublay on October 10, 1938, and an order for 50 aircraft followed in January 1939. Intended for use by the Armee de l’Air in French Indo China, they were to be powered by, 1030 hp GnomeRhone 14N39 14 cylinder radials and designated F.K.58A. Deliveries began in mid June 1939, and 17 were delivered within the next three months, of which the first four retained the Hispano Suiza powerplant, the other 13 being F.K.58As. However, due to inadequate production facilities, the small Koolhoven factory was not able to complete the French order. The construction of 10 French F.K.58As was sub contracted to SABCA in Belgium, but although the airframes had been completed when Germany invaded that country in 1940, their Gnome Rhone engines had not been delivered from France.
Following the first flight of a second Hispano powered prototype (PH AVA) on February 14, 1939, the Netherlands government in the following month ordered 36 F.K.58s, to be powered by 1080 hp Bristol Taurus III engines; but here again engine supply problems intervened, and Koolhoven was unable to complete any of the order for the Luchtvaartafdeling (Dutch air force). The production line and the second prototype were destroyed in a Luftwaffe air attack, the first prototype having already been lost in a crash in January 1940.
Thus the only operational F.K.58s were those supplied to the Armee de l’Air. Armed with four 7.5 mm (0.29 in) FN Browning machine guns, in two underwing fairings outboard of the main undercarriage legs, most of them were deployed by patrouilles de protection in May 1940, in defence of such towns as Aulnat, Caen, Clermont Ferrand, Cognac and La Rochelle. For a short time, they were among the Luftwaffe’s most cosmopolitan opponents, for these Dutch fighters with French engines and Belgian guns were often flown by Polish pilots.
F.K.58A
Span: 10.97 m (36 ft)
Length: 8.68 m (28 ft 51 in)
Gross weight: 2750 kg (6065 lb)
Maximum speed: 475 km/h (295 mph).
Koolhoven F.K.57
Executive plane, 1938
Koolhoven F.K.56
Military advanced trainer and scout, 1937
Koolhoven F.K.55
The prototype of the F.K.55 was a contra propelled fighter with many innovations.
A high performance fighter with retractable gear, the F.K55 was one of the highlights at the Paris Air Salon of 1936.
A second test flight prototype had been build and flown, but the project was delayed because priority was given to more conventional fighters.
Koolhoven F.K.54
Executive plane, first Koolhoven with retractable gear, 1937
Koolhoven F.K.53 ‘Junior’
Light private plane with side by side seats, 1936
