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The Bell ARH-70 was to be a reconnaissance armed helicopter, manufactured by Bell Helicopter for the United States Army’s Armed Reconnaissance Helicopter (ARH) program. Due to delays and increased program costs, the ARH-70 was cancelled in 2008 after four prototypes were produced. The development of the ARH-70 began in 2005, soon after they won the bid for the ARH program over Boeing. As a modified version of the Bell 407, the Bell ARH-70 was proposed to fulfill the needs as set out by the United States Army, all while only using off-the-shelf technology.

Aircraft Model Bell Arh 70 Details

Model No : Bell Arh 70
Aircraft Type : Military Helicopter
Manufacturer : Bell Helicopter
Country : United States
Manufactured : 2010 to: Onward
ICAO : NA
Avionics : NA
Engine : 1 × Honeywell HTS900-2 turboshaft
Power : 970 horse[Power]
Max Cruise Speed : 140 knots - 259 Km/h
Approach Speed : NA
Travel Range : 162 Nautical Miles - 300 Kilometers
Fuel Economy : 2.31 nautical mile / gallon - 1.130 kilometres / litre
Service Ceiling : 20,000 feet
Rate of Climb : NA
Take Off Distance : NA
Landing Distance : NA
Max Tak eOff Weight : 2,268 Kg - 5,000 lbs
Max Payload : 847 Kg - 1,867 lbs
Fuel Tank Capacity : 70 gallon - 265 litre
Baggage Volume : NA
Seats Economy/General Class : 6 seats
Seats Business Class : 0
Seats First Class : 0
Cabin Height : NA
Cabin Width : NA
Cabin Length : NA
Exterior Length : 10.57 metre - 34.68 feet
Tail Height : NA
Fuselage Diameter : NA
Wing Span Rotor Diameter : 10.67 metre - 35.01 feet
Wing Tips : NA
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For flight operation, the Bell ARH-70 was to feature a single Honeywell HTS900-2 turboshaft, capable of producing 970 horsepower to travel at a maximum speed of 140 knots. With a fuel tank capacity set at 70 gallons, the Bell ARH-70 would have a travel range of 160 nautical miles with a fuel economy equating to 2.31 nautical miles per gallon. For the seating and operation of the ARH-70, two pilots would be required, and up to six passengers could be transported at once. Altogether, the Bell ARH-70 would have a maximum takeoff weight of 5,000 lb, 2,598 lb being the empty weight of the helicopter itself.

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