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The tailplane also carried small endplate fins with much larger, curved, balanced rudders, placed directly in the slipstream of the engines to enhance low speed rudder authority. [ 1 ] The Twin-60 had a conventional, fixed undercarriage with the mainwheels on a single axle mounted on short, shock-absorbing legs from the lower fuselage longerons ...
The SlipStream Genesis is a family of American, strut-braced, high wing, pusher configuration, tricycle gear aircraft, produced in kit form, for amateur construction. Designed by Chuck Hamilton, the series were originally produced by Innovation Engineering of Davenport, Iowa and more recently by SlipStream International of Wautoma, Wisconsin .
Speedtwin Developments had taken over the aircraft in 2000 and in 2012 announced the new name of Comet 1. E2E stands for "Engineered to excel". At this time future developments including a retracting undercarriage, armament and turbo-prop engines were planned; the original idea of offering kits for home building had been withdrawn. [1]
The aircraft's installed power range is 52 to 100 hp (39 to 75 kW) and the standard engine is the 52 hp (39 kW) Rotax 503, although the 70 hp (52 kW) 2si 690 and 73 hp (54 kW) Subaru EA-81 engines have also been used. [1] [2] [3] The RW11 is only offered as plans and the designer estimates it will take 500 hours to complete the aircraft.
The Viking SF-2A Cygnet, also called the Sisler SF-2A Cygnet and the HAPI SF-2A Cygnet, is an American STOL amateur-built aircraft, designed by Bert Sisler and produced by Viking Aircraft LLC. The aircraft is supplied in the form of plans for amateur construction. The Cygnet first flew in 1973. [1] [2]
The twin fuselage configuration offers the advantage of a clean payload area underneath the wing centre section, without the need for exceptional ground clearance beneath the fuselages. Early concepts included the Conroy Virtus and Twin-fuselage Lockheed C-5 Galaxy Shuttle transport aircraft of 1974.
The aircraft's installed power range is 22 to 52 hp (16 to 39 kW) and the standard engine is the 38 hp (28 kW) Kawasaki 440A installed in tractor configuration. The 35 hp (26 kW) 2si 460 has also been used. [1] [2] [3] The RW9 is available only as plans and reported construction time is 150–175 hours. [1] [2] [3]
The EPB-1 is constructed with a wooden structure, with doped aircraft fabric covering. The landing gear is a monowheel, with a nose skid. [1] [2] The "A" model was described in the plans sold and retained the twin tip rudders of the EPB-1, although some were built with a single fin and rudder assembly attached to the cockpit rear.