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Depending on the supercharger fitted, engines were rated as low altitude (e.g.; Merlin 66, Griffon III), where the engine produced its maximum power below about 10,000 feet (3,000 m), medium altitude (Merlin 45), where the engine produced its maximum power up to about 20,000 feet (6,100 m), and high altitude (Merlin 70), where the engine produced its maximum power above about 25,000 feet ...
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 ...
1:3: 4 in: 101.60 mm P scale - ridable narrow gage park railroads, steamrollers, traction engines, Ball-jointed dolls, Super Dollfie, Dollfie Dream 1:2.4: 5 in: 127.00 mm Park railroads, where 15 in (381 mm) minimum gauge models are based on 3 ft (914 mm) narrow gauge prototypes 1:2: 6 in: 152.40 mm "My Size" (3 ft) fashion dolls: 1:1.8 ...
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 ...
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 ...
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.
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 ...
F.4/41 Spitfire with Griffon engine – written for Spitfire IV but amended to include Mk. XXI redesign. Preceded in introduction by Mk.s XII & XIV – some overlap with F.1/43 (q.v.) Supermarine Spitfire XXI: B.5/41 OR.106 Pressurised high-altitude bomber – evolved into B.3/42 (q.v.) Pressurised version of the Vickers Warwick III: E.6/41 OR.107