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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 fuselage is typically long and thin, usually with tapered or rounded ends to make its shape aerodynamically smooth. Most fixed-wing aircraft have a single fuselage. Others may have multiple fuselages, or the fuselage may be fitted with booms on either side of the tail to allow the extreme rear of the fuselage to be utilized.
The VK-30 was the predecessor of the Cirrus ST50, which had an almost-identical configuration to the VK-30, but included a larger ventral fin on the tail of the aircraft, a slightly larger fuselage, and was powered by a Pratt & Whitney Canada PT6-135 turboprop engine in place of the piston engine used in the VK-30.
At high engine speeds over-speeding and over-temperaturing (going beyond the maximum allowable) must be prevented to avoid turbine blade damage. [21] An example of an HMU, although called a Constant All Speed Control (CASC), was the Rolls-Royce/Lucas fuel control used on the Rolls-Royce Spey. It performed all the above functions as well as ...
The twin-boom configuration allows a large door to be placed at the rear of the fuselage, free from obstruction by the tail assembly, as on the Armstrong Whitworth AW.660 Argosy. However access to the rear door remains limited, especially for trucks backing up to it, and a high-mounted conventional rear fuselage is often preferred.
A narrow-body aircraft or single-aisle aircraft is an airliner arranged along a single aisle, permitting up to 6-abreast seating in a cabin less than 4 metres (13 ft) in width. In contrast, a wide-body aircraft is a larger airliner usually configured with multiple aisles and a fuselage diameter of more than 5 metres (16 ft), allowing at least ...
It was to use the DB 603 engine with 1,750 hp (1,300 kW) and had an estimated maximum speed of 740 km/h (460 mph). Only the G.56 was flown with this engine. A twin-fuselage version and a motorjet variant, the R.2005R were considered. On the R.2005R, speed could have been increased to 750 km/h (470 mph) but fuel consumption would have reached ...
Its landing gear is retractable. The delta configuration offers a relatively high cruise speed compared to conventional aircraft of the same weight and power. Its stall speed (70–75 mph) is relatively high for a small single-engine aircraft, and its configuration at touchdown is relatively nose-high. [4] Approach speeds of 100–110 mph are used.