Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:crew |
1
|
| gptkbp:emptyWeight |
8,188 kg
|
| gptkbp:engine |
gptkb:Pratt_&_Whitney_J57
|
| gptkbp:engineType |
turbojet
|
| gptkbp:firstFlight |
1955
|
| gptkbp:height |
4.8 m
|
| gptkbp:introduced |
1957
|
| gptkbp:length |
16.53 m
|
| gptkbp:manufacturer |
gptkb:Vought
|
| gptkbp:maximumSpeed |
Mach 1.86
|
| gptkbp:maxTakeoffWeight |
15,422 kg
|
| gptkbp:nickname |
gptkb:The_Last_of_the_Gunfighters
|
| gptkbp:numberBuilt |
1219
|
| gptkbp:primaryUser |
gptkb:United_States_Marine_Corps
gptkb:United_States_Navy |
| gptkbp:range |
1,500 km
|
| gptkbp:retired |
1976
|
| gptkbp:role |
carrier-based air superiority fighter
|
| gptkbp:serviceCeiling |
17,700 m
|
| gptkbp:successor |
F-4 Phantom II
|
| gptkbp:usedInConflict |
gptkb:Vietnam_War
|
| gptkbp:variant |
gptkb:Vought_F-8_Crusader
|
| gptkbp:weapon |
air-to-air missiles
20 mm cannons |
| gptkbp:wingspan |
10.87 m
|
| gptkbp:bfsParent |
gptkb:RF-8A
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
F-8A Crusader
|