f104c
F-104C is a fighter bomber, equipped withafterburning thrust of 7165 kg J79-GE-7 engine (military thrust 4540 kg), with limitedall-weather capability. July 24, 1958 firstflight, in September 1958 began delivery, delivery in the end of June 1959, a total of77 production. Equipped with 4 squadronsof the 479th tactical fighter wing. Thisaircraft equipped with 1 fixed type M61 20 mm Vulcan 6 gun, 5 pylon. Equipped withAN/ASG-14T2 fire control system. No.56-938 previous F-104 aircraft equipmentinterference coordination aura computingsight. Part of the F-104C (No.57-910) afterthe aircraft's optical sighting deviceremoved the optical distance measuringdevice, so the size of the aura is no longerchanged, its diameter is 50mil. Using radarto measure the target distance in firecontrol calculation. 1965 to 1967, part ofthe F-104C was sent to Vietnam to fight
Specifications
General Characteristics
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- Wingspan 37.7ft (11.5m)
- Length 45.8ft (14.0m)
- Height 14.0ft (4.3m)
- Empty Weight 9,026lbs (4,094kg)
- Loaded Weight 11,507lbs (5,219kg)
Performance
- Power/Weight Ratio 2.929
- Wing Loading 56.2lbs/ft2 (274.4kg/m2)
- Wing Area 204.8ft2 (19.0m2)
- Drag Points 4007
Parts
- Number of Parts 43
- Control Surfaces 5
- Performance Cost 365