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Encyclopedia > Bell Eagle Eye


Specifications

General Characteristics

  • Crew: none
  • Capacity: 200 lb (91 kg) payload
  • Length: 17 ft 11 in (5.46 m)
  • Wing span: 15 ft 2 in (4.63 m)
  • Main rotor diameter: 10 ft 0 in (3.05 m)
  • Height: ft in ( m)
  • Wing area: ft² ( m²)
  • Main rotor area: 157 ft² (14.6 m²)
  • Empty: lb ( kg)
  • Loaded: lb ( kg)
  • Maximum takeoff: 2,250 lb (1,023 kg)
  • Powerplant: 1 × Allison 250_C20B, 375 shp (280 kW)

Performance

  • Maximum speed: 225 mph (360 km/h)
  • Range: miles ( km)
  • Service ceiling: 14,500 ft (4,420 m)
  • Rate of climb: ft/min ( m/min)
  • Main rotor loading: lb/ft² ( kg/m&sup2:)
  • Wing loading: lb/ft² ( kg/m&sup2:)
  • Power/Mass: hp/lb ( kW/kg)

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  Results from FactBites:
 
News: Bell Eagle Eye completes autoland tests (724 words)
During the entire program, the Bell Eagle Eye executed all applicable demonstration objectives, and expanded the flight envelope of the aircraft substantially.
The Eagle Eye is a tiltrotor aircraft whose proprotors permit it to take-off and land vertically.
The Eagle Eye TR911X demonstrator is a 7/8 scale prototype aircraft built with more than 70% off-the-shelf manned-rated helicopter and common hardware parts.
  More results at FactBites »


 
 

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