Re: Combat Aircraft of the Indian Air Force IAF’s Boeing Chinook CH-47F
Not written about much but most certainly a very critical component of our vertical lift capability in the mountains is the ever green CH-47F. We now have 15 in service {or is it 10 in service and 5 yet to be delivered}. I sure wish we had 60 or 75.
The CH-47 or Chinook is a heavy lift twin rotor helicopter. It lifts a payload of 10.5 tonnes in its cabin or on three ventral cargo hooks for under slung loads. Within its cabin it can lift 33 fully equipped troops in two rows or 55 in ‘squeeze’ configuration. One RAF Chinook on a rescue mission lifted off with 128 souls on board!
In terms of the world’s four heavy lift military choppers {Mi-6, CH-53, Mi-26, CH-47} that served with squadrons the CH-47 is the lightest and the most widely used with over 1200 produced since its first flight almost 60 years ago in 1961.
Several design features indicate it is tailor made to carry military loads. The design with two rotors was chosen as it enables a full length cabin with a wide ramp door and drive in/roll on ability. The design affords the maximum length of usable cabin volume for a given overall length with rotors turning -- a critical factor when operating in mountains or out of jungle clearings. The four piece landing gear {quite unusual in a helicopter} allow it to land on soft ground without tilting over a common occurrence with tricycle landing gears when alighting on soft sand, soft snow or deep slush. The rear ramp can be kept open to accommodate lengthy cargo pieces which can protrude out in flight. The only condition being the centre of gravity envelope. The ramp itself operates in two parts -- the upper part can slide inside the lower half and serve as a observation or firing post or both halves can join together and act as one ramp.
The two main rotors design also gives the maximum swept area or disc area for a given overall length – a vital criterion in restricted mountain terrain flying. As most of you know rotor swept area {now Americanized to disc area} is aerodynamically akin to wing area of a fixed wing machine. The lower your disc loading {AUW/Swept Area} the better reserve lift safety you have. At 9.5 lbs/ sq foot the Chinook is moderately loaded. The Alouette Cheetah, the Queen of high altitude flying has a loading of ~5 lbs/sq foot!! The two turboshafts are mounted on the rear engine pylon and through a gearbox drive both rotors. In an emergency one engine too can drive both rotors.
This machine should do well in high altitude flying so needed by us. In addition to the disc loading it also has a good power to weight ratio of 0.28 {shp/lbs} at full load. This compares to 0.19 for the latest Mi-17 versions and the venerable Cheetah.
Length: 98 ft (30 m) ; Fuselage length: 52 ft (16 m)
Empty weight: 11. 14 tonnes; Max takeoff weight: 22.7 tonnes
Powerplant: 2 × Lycoming T55-GA-714A turboshaft engines, 4,733 shp each
Main rotor diameter: 2× 60 ft ; Main rotor area: 5,600 sq ft
Capacity:
33–55 troops or
24 stretchers and 3 attendants or
24,000 lb (10,886 kg) payload
Maximum speed: 170 knots , 310 km/h
Combat radius with full load: 200 nautical miles, 370 km
Ferry range: 1,216 nautical miles 2,252 km
Service ceiling: 20,000 feet ,6,100 metres
Initial rate of climb at sea level: 1,522 ft/min , 7.73 metres/second All pictures rediff.com. The last photo is of a US army Ch-47, included here to depict the ramp & aft cabin view.
Last edited by V.Narayan : 30th May 2020 at 21:22.
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