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[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.
The RW11 was designed for the US experimental homebuilt aircraft category or as a US FAR 103 Ultralight Vehicles two-seat ultralight trainer and first flown in 1996. [1] [2] [3] The airframe is constructed entirely from wood and covered with aircraft fabric. The landing gear is of conventional configuration with bungee suspension.
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 aerobatic aircraft is described as having a sharp stall, and ability to keep wings level using rudder alone. The Acroduster has shorter span and length, has larger ailerons than the Starduster Too, and has a stronger tail. [citation needed] The aircraft is constructed with fabric covered 4130 steel tube structure and spruce wing spars. Ribs ...
The aircraft's recommended engine power range is 60 to 82 hp (45 to 61 kW) and standard engines used include the 82 hp (61 kW) Volkswagen four-stroke powerplant. Construction time from the supplied kit is estimated as 1700–1800 hours. [1] [2] [4] The Cygnet won a design award at the EAA Annual Convention and Fly-In in 1973. [1]
Data from Terpstra General characteristics Crew: one Capacity: one passenger Length: 18 ft 10.25 in (5.75 m) Wingspan: 21 ft 8 in (6.60 m) Height: 6 ft 7.75 in (2.03 m) Wing area: 152 sq ft (14.12 m 2) Empty weight: 875 lb (397 kg) Gross weight: 1,520 lb (690 kg) Powerplant: 1 × Lycoming O-360 4-cylinder, air-cooled, horizontally-opposed piston aircraft engine, 180 hp (134 kW) Performance ...
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 ...
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