Search results
Results from the WOW.Com Content Network
Data from Jane's All the World's Aircraft 2010-11 General characteristics Capacity: 2 Length: 6.50 m (21 ft 4 in) Wingspan: 9.20 m (30 ft 2 in) Height: 2.15 m (7 ft 1 in) Wing area: 12.20 m 2 (131.3 sq ft) Empty weight: 265 kg (584 lb) Gross weight: 450 kg (992 lb) limited by European ultralight category Fuel capacity: 50 L (11.0 Imp gal, 13.2 US gal) Powerplant: 1 × Rotax 912 UL-DCDI air ...
(TL Ultralight, Hradec Králové) TL Ultralight TL-22 Duo; TL Ultralight TL-32 Typhoon; TL Ultralight TL-96 Star; TL Ultralight TL-132 Condor; TL Ultralight TL-232 Condor Plus; TL Ultralight TL-232 Power Condor; TL Ultralight TL-2000 StingCarbon; TL Ultralight TL-2000 StingSport; TL Ultralight TL-2000 Sting S3; TL Ultralight TL-3000 Sirius; TL ...
The engine is the largest reciprocating engine in the world. The 14-cylinder version first entered commercial service in September 2006 aboard the Emma Mærsk . The design is similar to the older RTA96C engine, but with common rail technology (in place of traditional camshaft , chain gear , fuel pump and hydraulic actuator systems).
The Stream is the company's fastest design to date. It was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, an enclosed cockpit with two-seats-in-tandem under a bubble canopy, retractable tricycle landing gear and a single engine in tractor configuration.
B Bailey Bailey C-7-R "Bull's Eye" 1927 = 140 hp 7RA. Bailey Aviation Main article: Bailey Aviation Bailey B200 Bailey Hornet Bailey V5 engine Baradat–Esteve (Claudio Baradat Guillé & Carlos Esteve) Baradat toroidal engine Basse und Selve Main article: Basse und Selve Basse und Selve BuS. 120 hp (125 mm × 160 mm (4.9 in × 6.3 in) 120-130 hp) Basse und Selve BuS.III 150 hp Basse und Selve ...
The aircraft replaces the Spyder's two-stroke engine with a Yuneec Power Drive 20 20 kW (27 hp) electric motor and two 28 lb (13 kg) Lithium polymer battery packs which provide a 40-minute endurance. The aircraft is intended to be developed into a commercially available kit and forecast to be available for under US$25,000.
The standard engine of the Condor Plus is the 48.5 kW (65 hp) Rotax 582 UL-DCDI, driving a two blade propeller, but the 59.7 kW (80 hp) Rotax 912 UL-DCDI or the 74.6 kW (100 hp) Rotax 912 ULS, both with three blade airscrews, are options. With the 912 ULS engine, the TL-232 is known as the Power Condor.
Data from Jane's All the World's Aircraft 2000/01 General characteristics Capacity: 2 Length: 5.90 m (19 ft 4 in) Wingspan: 10.70 m (35 ft 1 in) Height: 2.45 m (8 ft 0 in) Wing area: 15.20 m 2 (163.6 sq ft) gross Empty weight: 200 kg (441 lb) Max takeoff weight: 400 kg (882 lb) Powerplant: 1 × Rotax two cylinder two stroke Performance Maximum speed: 110 km/h (68 mph, 59 kn) Cruise speed: 90 ...