Armstrong Whitworth AW.660 Argosy | |
|---|---|
| 国 | 英国 |
| 役割 | 貨物輸送 |
| 初飛行 | 1959年1月8日 |
| 構築 | 74 |
ザ アームストロング・ホイットワース・アーゴシー は、戦後のイギリスの輸送/貨物機であり、航空会社アームストロング・ホイットワース・エアクラフトによって設計および製造された最後の航空機でした。AW.650 民間モデルと AW.660 軍用モデルは、内部設計番号は異なっていたが、ほとんどの実用上、同じ設計であり、両モデルとも「アーゴシー」の名称を共有していた。
ホーカー シドレー アーゴシー 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.
ソース： アームストロングホイットワースAW.660アーゴシーウィキペディア
| Hawker Siddeley Argosy Walk Around | |
|---|---|
| Photographer | Howard Mason |
| Localisation | Yankee Air Museum |
| Photos | 51 |
関連項目:
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) |
|---|---|
| 役割 | Medium-Range Transport / Cargo / Paratroop Carrier |
| メーカー | Armstrong Whitworth Aircraft (later Hawker Siddeley) |
| First Flight | March 4, 1961 (Military Variant) |
| 乗組員 | 4 (Pilot, Co-pilot, Navigator, Air Engineer) |
| 能力 | Up to 69 troops, 48 stretchers, or 13,000 kg (29,000 lb) of freight |
| 翼 | 35.05 m (115 ft 0 in) |
| 長さ | 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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