Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
demonstrator aircraft
|
| gptkbp:aircraftType |
gptkb:aircraft
|
| gptkbp:configuration |
delta wing
canard |
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:developedBy |
Dassault Rafale program
|
| gptkbp:engineType |
twin-engine
|
| gptkbp:firstFlight |
1986-07-04
|
| gptkbp:height |
5.34 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rafale A
|
| gptkbp:length |
15.80 m
|
| gptkbp:location |
Musée de l’Air et de l’Espace, Le Bourget, France
|
| gptkbp:manufacturer |
gptkb:Dassault_Aviation
|
| gptkbp:maxTakeoffWeight |
21,000 kg
|
| gptkbp:numberBuilt |
1
|
| gptkbp:powerplant |
2 × General Electric F404-GE-400 afterburning turbofans
|
| gptkbp:role |
gptkb:technology
|
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Dassault_Rafale
|
| gptkbp:usedFor |
aerodynamic research
engine testing avionics testing testing fly-by-wire controls |
| gptkbp:wingspan |
11.00 m
|
| gptkbp:bfsParent |
gptkb:Dassault_Rafale_(early_prototypes)
|
| gptkbp:bfsLayer |
8
|