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The fuselage of the Belfast was a relatively conservatively stressed cylinder of a conventional design. [19] It was developed with a target safe-life of 15,000 pressure cycles, which was fatigued tested using a complete fuselage immersed in a water tank. Fail-safe principles were used in the design of the large side door, rear ramp and door. [19]
On dark surfaces except upper surfaces July 1942 – January 1945; upper wings and fuselage sides of all Second Tactical Air Force (2 TAF) bombers and photo-reconnaissance Spitfires, January 1945 to early 1947. Upper and lower wings and fuselage sides of 2 TAF fighters (e.g.: Hawker Tempest) January 1945 to early 1947. [4] Ratio 4:8:9 (SEAC)
The fuselage (/ ˈ f juː z əl ɑː ʒ /; from the French fuselé "spindle-shaped") is an aircraft's main body section. It holds crew , passengers, or cargo . In single-engine aircraft, it will usually contain an engine as well, although in some amphibious aircraft the single engine is mounted on a pylon attached to the fuselage, which in turn ...
The Sopwith Triplane was a single seat fighter aircraft; it shared a considerable amount of its design features, such as its fuselage and empennage, with those of the earlier Pup. While the fuselage was structurally similar, Bruce notes that there were several areas of differences present. [3]
4 × AIM-7 Sparrow or Skyflash in fuselage recesses plus 2 × Sparrow / Skyflash on underwing pylons and 4 × AIM-9 Sidewinders on underwing shoulder rails; SUU-23/A gun pod on centreline pylon with up to 1,200 rounds (RAF aircraft only) [176] Strike. Up to 180 SNEB 68mm unguided rockets; Mix of 500lb, 750lb and 1000lb free-fall or retarded bombs
De Havilland nonetheless began a refit programme to strengthen the fuselage and wing structure, employing thicker-gauge skin and replacing the rectangular windows and panels with rounded versions, although this was not related to the erroneous 'square' window claim, as can be seen by the fact that the fuselage escape hatch cut-outs (the source ...
The Auster AOP.6 (Auster Model K) was designed as a successor to the Taylorcraft Auster V, it had a strengthened fuselage, increased all-up weight and a 145 hp (108 kW) de Havilland Gipsy Major 7 engine. It had a different appearance to the wartime Austers due to the lengthened landing gear struts (due to the larger propeller), and external non ...
The de Havilland DH.114 Heron is a small propeller-driven British airliner that first flew on 10 May 1950. It was a development of the twin-engine de Havilland Dove, with a stretched fuselage and two more engines. It was designed as a rugged, conventional low-wing monoplane with tricycle undercarriage that could be used on regional and commuter ...
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