Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:control_system |
fly-by-wire
|
| gptkbp:crew |
gptkb:1
|
| gptkbp:design_purpose |
research and development
|
| gptkbp:engine_type |
gptkb:turbofan_engine
|
| gptkbp:first_flight |
gptkb:1955
|
| gptkbp:height |
4.3 m
|
| gptkbp:hover_capability |
gptkb:true
|
| https://www.w3.org/2000/01/rdf-schema#label |
X-19
|
| gptkbp:invention |
2
|
| gptkbp:landing_gear |
tricycle landing gear
|
| gptkbp:length |
15.2 m
|
| gptkbp:manufacturer |
gptkb:Bell_Aircraft_Corporation
|
| gptkbp:max_speed |
1,000 km/h
|
| gptkbp:max_takeoff_weight |
6,000 kg
|
| gptkbp:notable_feature |
tilting wings
|
| gptkbp:range |
1,500 km
|
| gptkbp:retirement_year |
gptkb:1966
|
| gptkbp:role |
gptkb:aircraft
|
| gptkbp:significance |
first aircraft to achieve vertical takeoff and landing with jet propulsion.
|
| gptkbp:test_program_duration |
1955-1966
|
| gptkbp:vertical_takeoff |
gptkb:true
|
| gptkbp:wingspan |
12.2 m
|
| gptkbp:bfsParent |
gptkb:Joint_Service_Vertical_Takeoff/_Landing_Experimental_Program
|
| gptkbp:bfsLayer |
5
|