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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).
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
These engines were based on the Hemi engines, using the same blocks and crankshaft parts, but completely different cylinder heads, pushrods, exhaust manifolds and pistons. They were called Polyspheric or Poly engines, because they featured polyspherical-shaped (meaning "more than one sphere") combustion chambers .
(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 ...
Data from Kitplanes General characteristics Crew: one Capacity: one passenger and 520 lb (236 kg) useful load Length: 15 ft 0 in (4.56 m) Wingspan: 32 ft 0 in (9.76 m) Height: 7 ft 6 in (2.29 m) Wing area: 157 sq ft (14.60 m 2) Empty weight: 430 lb (195 kg) Max takeoff weight: 950 lb (431 kg) Powerplant: 1 × HKS 700E two-cylinder four-stroke, 60 hp (45 kW) Performance Maximum speed: 96 mph ...
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.
Compared to its predecessor, it featured a strengthened fuselage, longer nose, a vastly updated cockpit, and a more powerful (21.6 kN (4,850 lbf)) Lotarev DV-2 engine, allowing operation at higher weights and speeds (max speed 872 km/h (542 mph)). [96] [97] First flight on 30 September 1986. It was later designated as the Aero L-59.