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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 ...
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 Northstar engine is a family of high-performance 90° V engines produced by General Motors between 1993 and 2011. Regarded as GM's most technically complex engine, the original double overhead cam, four valve per cylinder, aluminum block/aluminum head V8 design was developed by Oldsmobile R&D, [citation needed] but is most associated with Cadillac's Northstar series.
TL-22 Duo: 1990s 50 (1998) Ultralight trike: TL-32 Typhoon: 1991 >200 Fabric covered high-wing ultralight aircraft: TL-96 Star: 1997 Composite low-wing ultralight aircraft TL-132 Condor: 1993 115 (2010) Fabric covered high-wing ultralight aircraft TL-232 Condor Plus: Fabric covered high-wing ultralight aircraft TL-2000 Sting: 2002
(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 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.
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.
The TL-3000 is a mostly composite aircraft with a carbon fibre wing and glass-and carbon-fibre fuselage. It shares many components with its TL-2000 Sting low wing stablemate. The high wing has a constant chord centre section and tapered outer panels with downturned tips and is braced to the lower fuselage with a pair of forward-leaning lift ...