Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:crew |
1
|
| gptkbp:developedBy |
gptkb:Eurofighter_Typhoon_program
|
| gptkbp:displayedAt |
gptkb:RAF_Museum_Cosford
|
| gptkbp:emptyWeight |
9,000 kg
|
| gptkbp:engine |
gptkb:Turbo-Union_RB199
|
| gptkbp:engineType |
Turbojet
|
| gptkbp:firstFlight |
1986-08-08
|
| gptkbp:height |
5.3 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
BAe EAP
|
| gptkbp:length |
15.6 m
|
| gptkbp:manufacturer |
gptkb:British_Aerospace
|
| gptkbp:maximumSpeed |
Mach 2
|
| gptkbp:maxTakeoffWeight |
13,000 kg
|
| gptkbp:numberBuilt |
1
|
| gptkbp:primaryUser |
gptkb:Royal_Aircraft_Establishment
|
| gptkbp:retired |
1991
|
| gptkbp:role |
gptkb:technology
|
| gptkbp:status |
retired
|
| gptkbp:testbedFor |
composite materials
fly-by-wire controls advanced aerodynamics canard-delta configuration |
| gptkbp:thrust |
40 kN
|
| gptkbp:wingspan |
11.0 m
|
| gptkbp:bfsParent |
gptkb:BAe_3201
|
| gptkbp:bfsLayer |
7
|