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The Excalibur was designed as "clone" [1] of the Quad City Challenger II aircraft. The company took the basic Challenger design and incorporated many changes, including mounting the engine upright allowing larger propellers and the Rotax gearbox to be mounted, lengthening the tailboom and enlarging the tail vertical surface to increase stability, shortening the ailerons and replacing control ...
The new design differed so much from the original Excalibur, that a different model designation was needed. It was first given the temporary designation L-104, then it was later officially designated the Model 49 or "Excalibur A". In time, the Model 49 would become a completely different aircraft from the original Model 44.
The M982 Excalibur (previously XM982) is a 155 mm extended-range guided artillery shell developed in a collaborative effort between the U.S. Army Research Laboratory (ARL) and the United States Army Armament Research, Development and Engineering Center (ARDEC). [4] The Excalibur was developed and/or manufactured by prime contractor Raytheon ...
Data from Challenger.ca General characteristics Crew: one Capacity: one passenger and 500 lb (227 kg) useful load Length: 20 ft (6.1 m) Wingspan: 31 ft 6 in (9.60 m) Height: 6 ft 0 in (1.83 m) Wing area: 177 sq ft (16.4 m 2) Empty weight: 460 lb (209 kg) Max takeoff weight: 960 lb (435 kg) Powerplant: 1 × Rotax 503 twin cylinder, inline, two stroke, piston aircraft engine, 50 hp (37 kW ...
Fieseler Fi 156C-2/C-3/D-1: Germany/Romania: Reconnaissance/liaison aircraft: 112 74 built by ICAR Retired after 1948 Focke-Wulf Fw 189A-2: Germany: Reconnaissance 2 In service 1943–1945 Gotha Go 145: Germany: Trainer 15 In service from 1939, retired after 1948 Gotha Go 150: Germany: Trainer 1 Requisitioned in 1941, retired after 1948 Gotha ...
The SA26 Merlin is a pressurized Excalibur fitted with a different Lycoming TIGO-540 6-cylinder geared piston engine. The TIGO 540 was used despite the fact that one of the reasons the IO-720 was used in the Excalibur was that the Queen Air series' IGSO-480 and IGSO-540 engines from the same manufacturer were so troublesome.
Data from Cliche & HKS General characteristics Type: Two cylinder, four-stroke aircraft engine Bore: 85 mm (3.3 in) Stroke: 60 mm (2.4 in) Displacement: 680 cc (41.49 cu in) Dry weight: 55 kg (121 lb) equipped with electrical system, electric starter, carburetors, gearbox, exhaust system, oil tank and cooler Components Valvetrain: two intake and two exhaust valves per cylinder Fuel type ...
In December 2010 the CEA-308, powered by the Jabiru 2200, set four FAI records for aircraft weighing less than 300 kg. It averaged 223 miles/hour for four runs over the 3-km low-altitude course [ 6 ] and 203 mph on a 100-km circuit.