Statements (71)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:bfsLayer |
6
|
| gptkbp:bfsParent |
gptkb:XV-15_A
gptkb:Hughes_X-18 |
| gptkbp:aircraft_operated |
gptkb:Robert_L._Mc_Culloch
gptkb:helicopter 2 hours advanced avionics fly-by-wire high maneuverability redundant systems thrust-to-weight ratio influenced future designs 6,000 lbs pioneered new technologies advanced stability systems compound helicopter multi-rotor design experimental VTOL aircraft experimental tilt rotor |
| gptkbp:cockpit |
tandem seating
|
| gptkbp:controls |
gptkb:helicopter
mechanical linkages |
| gptkbp:crew |
2
|
| gptkbp:design |
Bell engineers
improve VTOL efficiency tilt rotor |
| gptkbp:developer |
1962-1966
|
| gptkbp:elevation |
15,000 ft
|
| gptkbp:engine |
gptkb:Lycoming_T53
|
| gptkbp:features |
four rotors
|
| gptkbp:first_flight |
gptkb:1966
gptkb:NASA_Langley_Research_Center military applications several years operational testing recorded for analysis enhanced by design validated design concepts expanded VTOL capabilities stable hover successful hover tests vertical to horizontal transition |
| gptkbp:has_authority_over |
pilot operated
|
| gptkbp:height |
10 ft 0 in
|
| gptkbp:historical_context |
Cold War aviation research
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bell X-22
|
| gptkbp:innovation |
tilt rotor mechanism
|
| gptkbp:is_tested_for |
VTOL research
evaluation of VTOL capabilities |
| gptkbp:landing_gear |
tricycle gear
|
| gptkbp:length |
30 ft 0 in
|
| gptkbp:manufacturer |
gptkb:Bell_Aircraft_Corporation
|
| gptkbp:material |
aluminum
|
| gptkbp:max_speed |
200 knots
|
| gptkbp:max_takeoff_weight |
vertical landing
vertical takeoff |
| gptkbp:number_built |
gptkb:5
|
| gptkbp:operational_area |
military testing
|
| gptkbp:operational_range |
300 miles
|
| gptkbp:primary_user |
gptkb:military_unit
|
| gptkbp:propulsion |
turbine engines
|
| gptkbp:research_focus |
hover performance
|
| gptkbp:role |
gptkb:aircraft
|
| gptkbp:roll_rate |
30 degrees per second
|
| gptkbp:significance |
advanced rotorcraft technology
|
| gptkbp:status |
retired
|
| gptkbp:strikeouts |
cyclic pitch
|
| gptkbp:successor |
gptkb:V-22_Osprey
|
| gptkbp:surface |
elevons
|
| gptkbp:wingspan |
30 ft 0 in
|