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The Vickers Vanguard was a short/medium-range turboprop airliner designed and produced by the British aircraft manufacturer Vickers-Armstrongs.. The Vanguard was developed during the mid-to-late 1950s in response to a specification issued by British European Airways (BEA) for a 100-seat airliner; Vickers decided to design such an airliner as a follow-up to the existing Viscount series, the ...
Manufacturers have a team of technical engineers, writers and illustrators who compile information for these service manuals. Some companies create aftermarket repair manuals for the general public to purchase such as Clymer Haynes [1] and Triple M FZCO. [2] These manuals are also generally available as online auto repair manuals.
The Phase II Vanguard was powered, like the Phase I, by a 2088 cc 4-cylinder "wet sleeve" engine, now with a modestly increased compression ratio, and producing 68 hp. This engine could be modified by using an additional intake system and two single-barrel Solex carburettors, producing 90 hp. Typically, the Phase II engine was one Solex ...
Vanguard Big Block V-Twin 895cc Model with 895 cc (54.6 cu in) displacement, bore of 86 mm (3.4 in), a stroke of 78 mm (3.1 in) and a power output of 25 to 33 hp (19 to 25 kW) at 3600 rpm [1] [2] Vanguard Big Block V-Twin 993cc
Developed from the earlier Victoria with the introduction of a wider fuselage, the Vanguard was a 22-passenger twin-engined biplane. Originally built for the Air Ministry as the Type 62 the aircraft powered by two 450 hp Napier Lion engines first flew on 18 July 1923. [1]
This is an accepted version of this page This is the latest accepted revision, reviewed on 8 November 2024. British four-engined medium-range turboprop airliner, 1948 Viscount Cambrian Airways Vickers Viscount General information Type Turboprop airliner National origin United Kingdom Manufacturer Vickers-Armstrongs Status Retired Primary users British European Airways Capital Airlines Trans ...
The HP.80's crescent wing was tested on a ⅓-scale glider, the HP.87, and a heavily modified Supermarine Attacker, which was given the Handley Page HP.88 designation. The HP.88 crashed on 26 August 1951 after completing only about thirty flights and little useful data was gained during its brief two months of existence.
The XLR50 was a pump-fed liquid-propellant rocket engine burning RP-1 and LOX in a gas generator cycle developed by General Electric. [3] It was used to power the first stage of the Vanguard rockets on the Vanguard project.