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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 .
The aircraft's installed power range is 52 to 75 hp (39 to 56 kW) and the standard engine is the 52 hp (39 kW) Rotax 503, although the 70 hp (52 kW) 2si 540 has also been used. [ 1 ] [ 2 ] [ 3 ] The PT2S is only offered as plans and the designer estimates it will take 500 hours to complete the aircraft.
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 ...
Deflected slipstream is an approach to creating an aircraft that can take off and land vertically (), or at least with a very short runway ().The basic principle is to deflect the slipstream from one or more propellers approximately 90 degrees, to create an upward thrust for vertical takeoff and a downward air cushion for landing.
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 design was successful, and, following a first flight in September 1968, a large number of aircraft have been constructed by homebuilders. The aircraft are usually powered by converted Volkswagen air-cooled engines. [3] The VP-1 is a single-seat open-cockpit low-wing monoplane manufactured from spruce and plywood with fabric covered wings.
The first aircraft designed by Homer Kolb, it was ahead of its time and was not produced commercially until 1980, when the ultralight boom hit North America. [1] [2] The Flyer is a very light and simple aircraft with a standard empty weight of only 185 lb (84 kg). It features a completely open cockpit with the pilot exposed to the slipstream.
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. At least one two-place side-by-side seating version was built in Australia, and another as a motor glider. The standard wingspan is 25 ft (7.6 m), but versions ...