The Bell ARH-70A
Armed Reconnaissance Helicopter
Detect a threat. Destroy the threat. Save lives. Finite rules of engagement that have stood the test of time and hold true even today. While the rules have stood steadfast, never before has there been an emphasis on the capability to quickly identify and decidedly eliminate a threat, in an effort to ultimately save lives.
The new Bell Armed Reconnaissance Helicopter (ARH-70A) was developed to meet the U.S. Army's need for a fast, agile armed reconnaissance helicopter and meet it today, bringing 21st Century capability to the age-old rules of engagement.
With the capacity to expand potential, power and capability, the Bell ARH-70A is the perfect breed for ARH missions. With unmatched capability, the Bell ARH-70A is designed to shorten battles and save lives.
Versatile
The ARH-70A has:
- Modern, Common Avionics Architectrue System (CAAS)
- Digital glass cockpit
- Full-color multifunction displays
- Night vision capability
- Plug-and-play capability for network or systems of systems
Agile
The ARH-70A is powered by one Honeywell HTS900-2 turbine engine rated at 970 shp (723kW). This proven engine platform not only provides optimum performance, maneuverability and confidence for an array of missions.
Lethal
Not only can the ARH-70A track its prey, it can move in for the kill. It can be equipped with an array of weapons systems including: a 0.50-cal Gatling gun, a 7-tube 2.75" FFAR launcher or as many as 38 tubes at one time.
Transportable
Whether by road, sea or air, the ARH-70A provides simple, long-range deployability. It has been designed to occupy a minimal footprint for both storage and logistic efficiencies.
Specifications
Powerplant: |
One Honeywell HTS900-2 turbine engine rated at 970 shp (723 kW) |
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Dimensions: |
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Length: |
34 feet 8 inches (10.57 m) | |
Height: |
10 feet 11 inches (3.32 m) | |
Rotor: |
35 feet Dia. (10.67 m) | |
Weight: |
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| Useful load: | 1,868 lb. (847 kg) | |
Performance: |
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| Speed: | 161 mph (140 KTAS) max. 0-130 mph (0-113 KTAS) cruise |
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| Ceiling: | 20,000 feet (1,219m) | |
| Range: | >162 nm ( > 300 km) at 4K/95F |
The data set forth herein is preliminary and general in nature. Actual performance data of production aircraft may vary with conditions. For performance data and operating limitations for any specific flight mission, reference must be made to the approved flight manual, once available. Approved for public release, Public Affairs Office, U.S. Army Aviation and Missile command (AMSAM-PA) Reference Number: 250-2006
