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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 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 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armament and turbo-prop engines were planned; the original idea of offering kits for home building had been withdrawn.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 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 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 2-0-2 was the first airplane subjected to the CAA's then new 'Accelerated Service Test', introduced May 15, 1947. In this test, an airliner was to undergo a rigorous 150-hour test, attempting to squeeze one year's service into a week to 10 days of flying.
Data from Kitplanes, Purdy and RagWing General characteristics Crew: one Capacity: one passenger Length: 22 ft 0 in (6.71 m) Wingspan: 32 ft 0 in (9.75 m) Height: 7 ft 0 in (2.13 m) Wing area: 180 sq ft (17 m 2) Empty weight: 497 lb (225 kg) Gross weight: 1,200 lb (544 kg) Fuel capacity: 20 US gallons (76 litres) Powerplant: 1 × 2si 690 twin cylinder two stroke aircraft engine, 70 hp (52 kW ...