Lockheed F-104D
Lockheed F-104D Starfighter
The Lockheed F-104 Starfighter was the first operational interceptor capable of sustained speeds above Mach 2. Design work began in 1952 and the first test flights were flown in 1954. The F-104 was intended as a short-range point defense fighter with both single and two seat versions. The Starfighter was extensively exported and built under license in Canada, Europe, and Japan. The F-104D model is a two seat fully combat-capable trainer built for use by the U.S. Air Force’s Tactical Air Command between November 1958 and September 1959. A total of 21 were built. To make room for the second seat the F-104D gave up its internal gun but was given an enhanced ground strike capability and in-flight refueling.
| Wingspan | 21 ft 11 in. |
Wingspan |
| Length | 54 ft 9 in. |
Length |
| Height | 13 ft 6 in. |
Height |
| Weight | 24,388 (loaded) |
Weight |
| Max. Speed | Mach 2 |
Maximum Speed |
| Service Ceiling | 57,500 ft |
Service Ceiling |
| Range | 1,388 miles |
Range |
| Engines | General Electric J79-GE-7 with 15,800 pounds of thrust |
Engine |
| Crew | 2 |
Crew |
Manufacturer
Lockheed
Markings
156th Tactical Fighter Group, Puerto Rico Air National Guard, San Juan International Airport, Puerto Rico, 1974
Designation
F-104D
Serial Number
57-1323