BELL 360
Mission Scenarios
Highlights
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Rear
Front
Cockpit
INVICTUS
Relieves rotor lift demand, suppressing retreating blade stall for increased speed.
Lift-Sharing Wing
This strategy enables low-cost, rapid development and deployment, and significantly reduced cost-of-change throughout the aircraft’s lifecycle.
Modular OPEN systems Approach
Provides an optimized field of view and reduced crew exposure with full pilot functionality from either station.
Low Drag Tandem Cockpit
Blades designed for high speed, low life-cycle cost, and significant drag reduction. Robust, low-maintenance design based on the Bell 525’s efficient proven high speed (>200 knots in level flight), producible solution.
High Performance Rotor System
Trims aircraft pitch attitude to minimize drag enhancing the overall maneuverability.
Active Horizontal TAIL
Provides auxiliary power for ground maintenance and system checks and delivers supplemental horsepower to boost cruise-airspeed, dash-speed, hover payload, and autorotative performance.
Supplemental Power Unit (SPU)
Scenario 3
Scenario 2
Scenario 1
Target
BASE
230 nm from base
30 mins on target
Proven on the Bell V-280 Valor and Bell 525 Relentless, Bell's advanced digital flight control system harmonizes mature technologies for next-generation performance inclusive of pilot-optional operations.
Fly-by-Wire
Eliminates drag for high speed mission capability.
Retractable Weapons
Canted for payload increase and provides desirable pitch attitude at low speed enabling versatility for operations in any environment. Enhances cruise efficiency and maneuverability while suppressing retreating blade stall for increased speed.
Compact Ducted Tail Rotor
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