Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:crashLocation |
both prototypes lost in crashes
|
| gptkbp:engine |
gptkb:Pratt_&_Whitney_Canada_PW207D
|
| gptkbp:engineType |
turboshaft
|
| gptkbp:firstFlight |
2003
|
| gptkbp:height |
2.1 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Boeing X-50 Dragonfly
|
| gptkbp:length |
5.9 m
|
| gptkbp:manufacturer |
gptkb:DARPA
gptkb:Boeing |
| gptkbp:maximumSpeed |
370 km/h
|
| gptkbp:maxTakeoffWeight |
730 kg
|
| gptkbp:notableProject |
Canard Rotor/Wing (CRW)
|
| gptkbp:numberBuilt |
2
|
| gptkbp:primaryUser |
gptkb:DARPA
|
| gptkbp:programEndYear |
2006
|
| gptkbp:purpose |
demonstrate stopped rotor technology
|
| gptkbp:role |
gptkb:helicopter
|
| gptkbp:status |
cancelled
|
| gptkbp:type |
gptkb:helicopter
|
| gptkbp:wingspan |
7.0 m
|
| gptkbp:bfsParent |
gptkb:US_military_X-plane_program
gptkb:X-50 |
| gptkbp:bfsLayer |
7
|