Srpskohrvatski / srpskohrvatski

Armstrong Whitworth AW.660 Argosy

ZemljaVelike britanije
UloguPrevoz tereta
Prvi let8. januar 1959.
Izgradio74

Čaj Srpskohrvatski / srpskohrvatski bio je britanski posleratni transportni / teretni avion, to je bio konačni avion koji će biti dizajniran i proizveden od strane vazduhoplovne kompanije Armstrong Vhitvorth Aircraft. Iako su dobili različite unutrašnje brojeve dizajna, AV.KSNUMKS civilni i AV.KSNUMKS vojni modeli su, za većinu praktičnih razloga, isti dizajn, dok su oba modela takođe delili ime "Argosi".

Hawker Siddelei Argosy E Mk 1: During 1963, Hawker Siddeley Group dropped the names of its component companies, rebranding its products under the Hawker Siddeley banner. To meet a requirement for a RAF flight inspection aircraft, nine Argosy C.1s were modified in 1971 as the Argosy E.1. These were a regular sight at British military airfields, being operated by 115 Squadron until they were replaced by the Hawker Siddeley Andover during 1978.

Izvor: Armstrong Whitvorth AW.660 Argosy na Vikipediji
Hawker Siddeley Argosy Walk Around
PhotographerHoward Mason
LocalisationYankee Air Museum
Photos51
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General Characteristics (AW.660 C Mk 1)

The Armstrong Whitworth AW.660 Argosy was a British four-engine turboprop transport aircraft. Developed from the civil AW.650, the military AW.660 served as a medium-range transport, paratroop, and supply aircraft for the Royal Air Force (RAF). Its distinctive “pod-and-boom” structure with a high-set cockpit and rear clamshell doors allowed for easy, double-end loading, earning it the nickname, the “Whistling Wheelbarrow.”

Property Typical Value (AW.660 C Mk 1)
Ulogu Medium-Range Transport / Cargo / Paratroop Carrier
Proizvođača Armstrong Whitworth Aircraft (later Hawker Siddeley)
First Flight March 4, 1961 (Military Variant)
Posada 4 (Pilot, Co-pilot, Navigator, Air Engineer)
Kapacitet Up to 69 troops, 48 stretchers, or 13,000 kg (29,000 lb) of freight
Raspon krila 35.05 m (115 ft 0 in)
Dužina 26.44 m (86 ft 9 in)
Max Takeoff Weight 47,627 kg (105,000 lb)

Design and Powerplant

  • Engines: Four Rolls-Royce Dart Mk 101 turboprop engines.
  • Power Output (each): Approximately 1,840 kW (2,470 shp) equivalent horsepower.
  • Propellers: Four-bladed Rotol propellers.
  • Design Concept: The twin-boom arrangement was adopted to provide an unobstructed cargo compartment with loading doors at both the front and rear of the fuselage, allowing for simultaneous or straight-through loading.
  • Military Modifications: The AW.660 military variant differed from the civil AW.650 by featuring a sealed nose door (for weather radar), clamshell-style rear doors with an integral loading ramp, paratroop doors, and increased fuel capacity for double the range.
  • Cargo Handling: Utilized a “Rolomat” system of rollers and pallets to facilitate rapid loading and unloading without external lifting equipment.

Performance and Capabilities

  • Maximum Speed: Up to 460 km/h (286 mph, 248 knots).
  • Cruise Speed: Approximately 452 km/h (281 mph, 244 knots).
  • Service Ceiling: 6,400 m (21,000 ft).
  • Range: Approximately 3,219 km (2,000 mi, 1,738 nmi).
  • Key Capability: Could carry vehicles like the Saracen or Ferret armoured cars, or the 105 mm howitzer.
  • Later Variants: Some aircraft were converted to the Argosy E.1 for electronic calibration missions for the RAF.

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