Mitsubishi F-1 (Supersonic Rei-Sen) Technical Specifications
Service Year: 1978
Type: Strike / Anti-Ship Fighter Aircraft
National Origin: Japan
Manufacturer(s): Mitsubishi Heavy Industries / Fuji Heavy Industries - Japan
Production Total: 77
Structural (Crew Space, Dimensions and Weights)
Operating Crew (Typical): 1
Overall Length: 58.56 feet (17.85 meters)
Overall Width: 25.85 feet (7.88 meters)
Overall Height: 14.70 feet (4.48 meters)
Weight (Empty): 14,017 lb (6,358 kg)
Weight (MTOW): 30,203 lb (13,700 kg)
Installed Power and Standard Day Performance
Propulsion: 2 x Ishikawajima-Harima TF40-IHI-801A afterburning turbofans generating 7,305lbs of thrust each.
Maximum Speed: 1,056 mph (1,700 kph; 918 knots)
Maximum Range: 217 miles (350 km)
Service Ceiling: 50,000 feet (15,240 meters; 9.47 miles)
Rate-of-Climb: 35,000 feet-per-minute (10,668 m/min)
Armament / Mission Payload
1 x 20mm JM61 Vulcan 6-barreled internal cannon
2 x AIM-9L OR Mitsubishi AAM-1 air-to-air missiles (on wingtip mounts).
2 x ASM-1 anti-ship missiles, rocket pods or conventional drop bombs (500lbs/750lbs).
2 x Jettisonable fuel stores as required
Global Operators / Customers
Model Variants (Including Prototypes)
F-1 - Base Series Designation; introduction in 1978 and 77 examples produced.