Specifications
| Primary Function | Tactical fighter. |
| Contractor | McDonnell Douglas Corp. |
| Power Plant | Two Pratt & Whitney F100-PW-100 turbofan engines with afterburners. |
| Thrust | (C/D models) 25,000 pounds each engine ( 11,250 kilograms). |
| Length | 63 feet, 9 inches (19.43 meters). |
| Height | 18 feet, 8 inches (5.69 meters). |
| Wingspan | 42 feet, 10 inches (13.06 meters) |
| Speed | 1,875 mph (Mach 2.5-plus at sea level). |
| Ceiling | 65,000 feet (19,697 meters). |
| Maximum Takeoff Weight | (C/D models) 68,000 pounds (30,600 kilograms). |
| Range | 3,450 miles (3,000 nautical miles) ferry range with conformal fuel tanks and three external fuel tanks. |
| Armament | 1 - M-61A1 20mm multibarrel internal gun, 940 rounds of ammunition 4 - AIM-9L/M Sidewinder and 4 - AIM-7F/M Sparrow missiles, or combination of AIM-9L/M, AIM-7-F/M and AIM-120 missiles. |
| Crew | F-15A/C: one. F-15B/D: two. |
| Date Deployed | July 1972 |
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