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Data from L-39 Next Generation web page General characteristics Crew: 2 Length: 11.83 m (38 ft 10 in) Wingspan: 9.37 m (30 ft 9 in) Airfoil: NACA 64A012 Empty weight: 3,100 kg (6,834 lb) Max takeoff weight: 5,800 kg (12,787 lb) Rear view of a L-39 Skyfox and its Williams FJ44 engine Powerplant: 1 × Williams International FJ44-4M turbofan engine, 16.89 kN (3,800 lbf) thrust Performance Maximum ...
Barrel engine 1 built bench tests only Salmson B 2 x 7-cyl barrel 1910 75 mm (2.953 in) 125 mm (4.921 in) 7.7 L (469.88 cu in) 37.285 kW (50 hp) at 800rpm 1 built bench tests only. Salmson C 2 x 7-cyl barrel 1910 85 mm (3.346 in) 95 mm (3.740 in) 8 L (488.19 cu in) 44.74 kW (60 hp) at 1100rpm 1 built with rotary inlet valves. Salmson D 2 x 7 ...
The Tango 2 was developed from the 1983 Aero Mirage TC-2 design. [4] The Tango 2 is a side-by-side two-seat composite aircraft that can be flying in as little as 1000 hours of build time. Current aircraft have been built with engines ranging from the 150 HP O-320 Lycoming to the Geared Drives 205 hp EcoTech 2.2 liter supercharged Cobalt SS ...
The standard engine used is the 50 hp (37 kW) Rotax 503 two-stroke powerplant, which gives a standard day, sea level takeoff distance of 100 ft (30 m) and a landing roll of 150 ft (46 m). [ 1 ] The Mohawk has a typical empty weight of 450 lb (200 kg) and a gross weight of 1,000 lb (450 kg), giving a useful load of 550 lb (250 kg).
Approaching the 2,000th [2] The Honeywell HTF7000 is a turbofan engine produced by Honeywell Aerospace . Rated in the 6,540–7,624 lbf (29.09–33.91 kN) range, the HTF7000 is used on the Bombardier Challenger 300 /350, Gulfstream G280 , Embraer Legacy 500 /450 and the Cessna Citation Longitude .
[1] [2] [4] The Pulsar Series II has a typical empty weight of 660 lb (300 kg) and a gross weight of 1,200 lb (540 kg), giving a useful load of 540 lb (240 kg). With full fuel of 17 U.S. gallons (64 L; 14 imp gal) the payload for the pilot, passengers and baggage is 438 lb (199 kg).
Data from Aerolite 103 website & KitPlanes General characteristics Crew: one Length: 17 ft 0 in (5.19 m) Wingspan: 26 ft 10 in (8.18 m) Height: 6 ft 5 in (1.96 m) Wing area: 124 sq ft (11.54 m 2) Empty weight: 275 lb (125 kg) Max takeoff weight: 600 lb (272 kg) Powerplant: 1 × Rotax 447 fixed pitch, 40 hp (30 kW) Performance Maximum speed: 70 mph (113 km/h, 61 kn) Cruise speed: 63 mph (102 km ...
Data from Adam Aircraft and The Incomplete Guide to Airfoil Usage General characteristics Crew: one Capacity: five passengers Length: 37 ft 6 in (11.43 m) Wingspan: 44 ft 0 in (13.41 m) Height: 9 ft 7 in (2.92 m) Airfoil: NASA LS(1)-0417 Empty weight: 5,350 lb (2,427 kg) Gross weight: 7,000 lb (3,175 kg) Fuel capacity: 230 gal (872 litres) Powerplant: 2 × Teledyne Continental TSIO-550E, 350 ...