Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:armament |
gptkb:GAU-12/U_25_mm_rotary_cannon
|
| gptkbp:configuration |
single-engine
canard pusher propeller |
| gptkbp:crew |
1
|
| gptkbp:designer |
gptkb:Burt_Rutan
|
| gptkbp:emptyWeight |
2,250 lb (1,021 kg)
|
| gptkbp:engine |
gptkb:Pratt_&_Whitney_Canada_JT15D-1_turbofan
|
| gptkbp:firstFlight |
1989
|
| gptkbp:height |
7 ft 10 in (2.39 m)
|
| gptkbp:length |
25 ft 2 in (7.67 m)
|
| gptkbp:manufacturer |
gptkb:Scaled_Composites
|
| gptkbp:maximumSpeed |
414 mph (666 km/h)
|
| gptkbp:maxTakeoffWeight |
3,500 lb (1,588 kg)
|
| gptkbp:purpose |
gptkb:Close_Air_Support_(CAS)
|
| gptkbp:range |
1,200 mi (1,900 km)
|
| gptkbp:role |
gptkb:aircraft
|
| gptkbp:status |
gptkb:prototype
|
| gptkbp:thrust |
2,200 lbf (9.8 kN)
|
| gptkbp:wingspan |
23 ft 10 in (7.26 m)
|
| gptkbp:bfsParent |
gptkb:Burt_Rutan
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rutan ARES
|