Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:trainer_aircraft
|
| gptkbp:armament |
gptkb:AIM-9_Sidewinder
bombs rocket pods 20 mm JM61A1 Vulcan cannon |
| gptkbp:countryOfOrigin |
gptkb:Japan
|
| gptkbp:crew |
2
|
| gptkbp:developedBy |
gptkb:Mitsubishi_F-1
|
| gptkbp:engine |
Turbomeca/SNECMA Larzac (Ishikawajima-Harima TF40-801A)
|
| gptkbp:engineType |
twin turbojet
|
| gptkbp:firstFlight |
20 July 1971
|
| gptkbp:height |
4.43 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mitsubishi T-2 (production)
|
| gptkbp:introduced |
1975
|
| gptkbp:length |
17.85 m
|
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:maximumSpeed |
Mach 1.6
|
| gptkbp:numberBuilt |
90
|
| gptkbp:primaryUser |
gptkb:Japan_Air_Self-Defense_Force
|
| gptkbp:retired |
2006
|
| gptkbp:role |
supersonic jet trainer
|
| gptkbp:status |
retired
|
| gptkbp:usedFor |
light attack
weapons training advanced pilot training |
| gptkbp:wingspan |
7.88 m
|
| gptkbp:bfsParent |
gptkb:Mitsubishi_T-2_(early_prototypes)
|
| gptkbp:bfsLayer |
7
|