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The Jurca MJ-10 Spitfire is a sport aircraft designed by Marcel Jurca in France as a replica of the Supermarine Spitfire and marketed for homebuilding. Plans for two versions were produced, the MJ-10, at 3/4 scale, and the MJ-100, at full-scale. Construction throughout is of wood, and the builder may choose to complete the aircraft with either ...
The use of these prefixes did not change according to the wings, which could be fitted with "clipped" tips, reducing the wingspan to about 32 ft 6 in (9.9 m) (this could vary slightly), or the "pointed" tips which increased the wingspan to 40 ft 2 in (12.29 m).
At the time the record of 352 mph (566 km/h) was held by Howard Hughes flying a Hughes H-1 racing aircraft. [nb 6] Although an early Spitfire I was capable of 362 mph (583 km/h), this was at a full-throttle height of 16,800 ft (5,100 m); the regulations for the world speed record demanded that the aircraft fly a 1.86-mile (2.99 km) course at an ...
Data from Supermarine Aircraft General characteristics Length: 23 ft 9 in (7.24 m) Wingspan: 27 ft 8 in (8.43 m) Height: 6 ft 9 in (2.06 m) Wing area: 122 sq ft (11.3 m 2) Empty weight: 992 lb (450 kg) Gross weight: 1,785 lb (810 kg) Powerplant: 1 × General Motors-Isuzu V-6 liquid-cooled piston engine, 226 hp (169 kW) Propellers: 3-bladed Ivoprop composite propeller Performance Maximum speed ...
Over the course of 4 months the Spitfire completed a number of flight routes, flying over 250 NHS and HSC sites across the United Kingdom in an effort to thank medical & health workers for their on-going fight against the virus. Simultaneously, the general public was able to donate money to 'The NHS Spitfire' project, with a nominated name from ...
The Mk XIV differed from the Mk XII in that the longer, two-stage supercharged Griffon 65, producing 2,050 hp (1,528 kW), was mounted 10 inches (25.4 cm) further forward. The top section of the engine bulkhead was angled forward, creating a distinctive change of angle to the upper cowling's rear edge.
In combination with the wing tanks this gave a total internal capacity of 122 gal (554.6 L), a near 50% increase over the 85 gal (386.4 L) carried by earlier Spitfire marks. In addition a 13 gal (64 L) fuel tank was fitted in each wing leading edge between the wingroot and the inner gun-bay.
Data from Jane's All the World's Aircraft 1988-89 General characteristics Crew: 1 Length: 19 ft 3 in (5.87 m) Wingspan: 22 ft 1 + 1 ⁄ 2 in (6.74 m) Height: 5 ft 8 in (1.73 m) Wing area: 87.0 sq ft (8.08 m 2) Airfoil: root: NACA 2213.2 ; tip: NACA 2206 Empty weight: 805 lb (365 kg) Gross weight: 1,100 lb (499 kg) Fuel capacity: 10 imp gal (12 US gal; 45 L) Powerplant: 1 × Continental O-200 4 ...