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BOEING CH-47 CHINOOK
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The Boeing CH-47 Chinook is an American twin-engined, tandem rotor, heavy-lift helicopter developed by American rotorcraft company Vertol and manufactured by Boeing Vertol (later known as Boeing Rotorcraft Systems). The CH-47 is among the heaviest lifting Western helicopters. Its name, Chinook, is from the Native American Chinook people of modern-day Washington state.

The Chinook was originally designed by Vertol, which had begun work in 1957 on a new tandem-rotor helicopter, designated as the Vertol Model 107 or V-107. Around the same time, the United States Department of the Army announced its intention to replace the piston engine-powered Sikorsky CH-37 Mojave with a new, gas turbine-powered helicopter. During June 1958, the U.S. Army ordered a small number of V-107s from Vertol under the YHC-1A designation; following testing, it came to be considered by some Army officials to be too heavy for the assault missions and too light for transport purposes. While the YHC-1A would be improved and adopted by the U.S. Marine Corps as the CH-46 Sea Knight, the Army sought a heavier transport helicopter, and ordered an enlarged derivative of the V-107 with the Vertol designation Model 114. Initially designated as the YCH-1B, on 21 September 1961, the preproduction rotorcraft performed its maiden flight. In 1962, the HC-1B was redesignated CH-47A under the 1962 United States Tri-Service aircraft designation system.

The Chinook possesses several means of loading various cargoes, including multiple doors across the fuselage, a wide loading ramp located at the rear of the fuselage, and a total of three external ventral cargo hooks to carry underslung loads, as well. Capable of a top speed of 170 knots (196 mph, 315 km/h), upon its introduction to service in 1962, the helicopter was considerably faster than contemporary 1960s utility helicopters and attack helicopters, and is still one of the fastest helicopters in the US inventory. Improved and more powerful versions of the Chinook have also been developed since its introduction; one of the most substantial variants to be produced was the CH-47D, which first entered service in 1982; improvements from the CH-47C standard included upgraded engines, composite rotor blades, a redesigned cockpit to reduce workload, improved and redundant electrical systems and avionics, and the adoption of an advanced flight control system. It remains one of the few aircraft to be developed during the early 1960s – along with the fixed-wing Lockheed C-130 Hercules cargo aircraft – that had remained in both production and frontline service for over 50 years.

The military version of the helicopter has been subject to numerous export sales from nations across the world, typically using it as heavy-lift rotorcraft in a military context; the U.S. Army and the Royal Air Force have been its two largest users. The civilian version of the Chinook is the Boeing Vertol 234. It has been used for a variety of purposes by a range of different civil operators, having often been used for passenger and cargo transport, along with niche roles such as aerial firefighting and to support various industrial activities, including logging, construction, and oil extraction.

General characteristics

  • Crew: three (pilot, copilot, flight engineer or loadmaster)
  • Capacity:
    • 33–55 troops or
    • 24 litters and 3 attendants or
  • Payload: 24,000 lb (10,886 kg)
  • Length: 98 ft 10 in(30.1 m)
  • Fuselage length: 52 ft (15.85 m)
  • Fuselage width: 12 ft 5 in(3.78 m)
  • Rotor diameter: 60 ft  (18.3 m)
  • Height: 18 ft 11 in (5.7 m)
  • Disc area: 5,600 ft2 (520 m2)
  • Empty weight: 24,578 lb (11,148 kg)
  • Max. takeoff weight: 50,000 lb (22,680 kg)
  • Powerplant: 2 × Lycoming T55-GA-714A turboshaft, 4,733 shp (3,529 kW) each

Performance

  • Maximum speed: 170 knots (196 mph, 315 km/h)
  • Cruise speed: 160 kt (184 mph, 296 km/h)
  • Range: 400 nmi (450 mi, 741 km)
  • Combat radius: 200 nmi (230 mi, 370 km)
  • Ferry range: 1,216 nmi (1,400 mi, 2,252 km)
  • Service ceiling: 20,000 ft (6100 m)
  • Rate of climb: 1,522 ft/min (7.73 m/s)
  • Disc loading: 9.5 lb/ft2 (47 kg/m2)
  • Power/mass: 0.28 hp/lb (460 W/kg)

Photos credits: Spot'Air

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