Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:configuration |
tail-sitter
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:crew |
1
|
| gptkbp:engineType |
turboprop
|
| gptkbp:firstFlight |
1954
|
| gptkbp:height |
35 ft 0 in (10.67 m)
|
| gptkbp:length |
32 ft 8 in (9.96 m)
|
| gptkbp:manufacturer |
gptkb:Lockheed_Martin
|
| gptkbp:maximumSpeed |
578 km/h (359 mph)
|
| gptkbp:maxTakeoffWeight |
16,270 lb (7,380 kg)
|
| gptkbp:nickname |
gptkb:fish
|
| gptkbp:numberBuilt |
1
|
| gptkbp:plannedArmament |
4 × 20 mm cannon
folding-fin rockets |
| gptkbp:powerplant |
Allison YT40-A-14 turboprop
|
| gptkbp:primaryUser |
gptkb:United_States_Navy
|
| gptkbp:projectCancelled |
1955
|
| gptkbp:role |
gptkb:VTOL_fighter
|
| gptkbp:status |
gptkb:prototype
|
| gptkbp:testLocation |
gptkb:Edwards_Air_Force_Base
|
| gptkbp:wingspan |
30 ft 0 in (9.14 m)
|
| gptkbp:bfsParent |
gptkb:Advanced_Development_Programs_(Skunk_Works)
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Lockheed Martin XFV
|