Statements (32)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:armament |
gptkb:PL-2_air-to-air_missile
gptkb:PL-5_air-to-air_missile bombs 23 mm twin-barrel cannon unguided rockets |
| gptkbp:basedOn |
gptkb:Mikoyan-Gurevich_MiG-21
|
| gptkbp:countryOfOrigin |
gptkb:China
|
| gptkbp:crew |
1
|
| gptkbp:engineType |
single turbojet
|
| gptkbp:exportedTo |
gptkb:Bangladesh
gptkb:Iran gptkb:Myanmar gptkb:Pakistan gptkb:Sri_Lanka |
| gptkbp:firstFlight |
May 1990
|
| gptkbp:height |
4.1 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
歼-7E
|
| gptkbp:introduced |
1993
|
| gptkbp:length |
14.885 m
|
| gptkbp:manufacturer |
gptkb:Chengdu_Aircraft_Corporation
|
| gptkbp:maximumSpeed |
Mach 2.0
|
| gptkbp:maxTakeoffWeight |
8,862 kg
|
| gptkbp:notableFeature |
double-delta wing design
|
| gptkbp:primaryUser |
gptkb:People's_Liberation_Army_Air_Force
|
| gptkbp:retired |
gptkb:People's_Liberation_Army_Air_Force
|
| gptkbp:role |
air superiority fighter
|
| gptkbp:status |
retired (in China)
|
| gptkbp:successor |
gptkb:JF-17_Thunder
|
| gptkbp:wingspan |
8.32 m
|
| gptkbp:bfsParent |
gptkb:歼-7战斗机
|
| gptkbp:bfsLayer |
7
|