Search results
Results From The WOW.Com Content Network
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". 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 ...
[1] [2] 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.
Data from Cliche and SlipStream General characteristics Crew: one Capacity: one passenger Length: 19 ft 4 in (5.89 m) Wingspan: 30 ft 8 in (9.35 m) Height: 6 ft 3.5 in (1.918 m) Wing area: 154 sq ft (14.3 m 2) Empty weight: 465 lb (211 kg) Gross weight: 1,100 lb (499 kg) Fuel capacity: 10 US gallons (38 litres) Powerplant: 1 × Rotax 503 twin cylinder, two-stroke aircraft engine, 50 hp (37 kW ...
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 Edgley EA-7 Optica is a British light aircraft designed for low-speed observation work, and intended as a low-cost alternative to helicopters.The Optica has a loiter speed of 130 km/h (70 kn; 81 mph) and a stall speed of 108 km/h (58 kn; 67 mph).
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 ...
In 1960, former Helio company engineer Joseph W. Gigante (1916-2012) designed a twin-engine conversion of the Sea Bee and founded United Consultants Corp in Norwood, Massachusetts, to undertake the manufacturing work on the UC-1 Twin Bee. [1] The first aircraft flew in 1962 and the type certificate was awarded on 25 June 1965. 23 production ...
Data from Kitplanes, Purdy and RagWing General characteristics Crew: one Capacity: one passenger Length: 18 ft 0 in (5.49 m) Wingspan: 28 ft 0 in (8.53 m) Height: 6 ft 6 in (1.98 m) Wing area: 123.8 sq ft (11.50 m 2) Empty weight: 420 lb (191 kg) Gross weight: 850 lb (386 kg) Fuel capacity: 10 US gallons (38 litres) Powerplant: 1 × Rotax 503 twin cylinder two stroke aircraft engine, 52 hp (39 ...