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Data from Jane's All The World's Aircraft 1982–83 General characteristics Crew: 1 Length: 18 ft 0 in (5.49 m) Wingspan: 24 ft 0 in (7.32 m) Height: 5 ft 1.5 in (1.562 m) Wing area: 100 sq ft (9.3 m 2) Airfoil: NACA 4412 Empty weight: 440 lb (200 kg) Max takeoff weight: 750 lb (340 kg) Powerplant: 1 × Volkswagen 4-cylinder air-cooled horizontally-opposed piston engine, 40 hp (30 kW ...
In June 1989 the Venture set three FAI speed records for piston aircraft weighing less than 1000 kg: 331 miles/hour average for four 3-km runs at low altitude [7] (beat by the Nemesis NXT in 2008) 305 mph for a 100-km circuit [8] 284 mph for a 1000-km circuit [9] The 100-km and 1000-km records still stand in 2023.
The Cameron P-51G (originally Cameron Grand 51) is an American two-seat turboprop representation of the 1940s North American P-51 Mustang, designed and built by Cameron & Sons Aircraft of Coeur d'Alene, Idaho for sale as completed aircraft or kits for amateur construction. [1]
Data from Sport Aviation, Plane & Pilot and Purdy General characteristics Crew: one Capacity: one passenger in tandem seating Length: 22 ft 5 in (6.83 m) Wingspan: 35 ft 3 in (10.74 m) Height: 6 ft 8 in (2.03 m) Wing area: 178.5 sq ft (16.58 m 2) Airfoil: USA 35B Empty weight: 695 lb (315 kg) Gross weight: 1,400 lb (635 kg) Fuel capacity: 12 US Gallons, 45.42 litres Powerplant: 1 × Lycoming O ...
[7] [b] Even the cost of operation would be extremely low, offering fuel efficiency of 38 mpg ‑US (16 km/L). With the wings removed, the aircraft could be packed into a small custom trailer, allowing it to be towed away by car for storage in a garage, and from there to any suitable flat area for takeoff. [4] [8]
The 230 hp (172 kW) engine gives the aircraft a sea level, standard day takeoff distance of 150 ft (46 m) and a landing distance of 300 ft (91 m). [ 1 ] [ 2 ] The V6 STOL has a typical empty weight of 1,200 lb (540 kg) and a gross weight of 2,200 lb (1,000 kg), giving a useful load of 1,000 lb (450 kg).