Mikoyan MiG 1.42 / 1.44 / MFI Technical Specifications
Service Year: 1999
Type: Technology Demonstrator
National Origin: Russia
Production Total: 3
Structural (Crew Space, Dimensions and Weights)
Operating Crew (Typical): 1
Overall Length: 62.34 feet (19 meters)
Overall Width: 49.21 feet (15.00 meters)
Overall Height: 14.76 feet (4.50 meters)
Weight (Empty): 39,683 lb (18,000 kg)
Weight (MTOW): 77,162 lb (35,000 kg)
Installed Power and Standard Day Performance
Propulsion: 2 x Saturn/Lyulka AL-41F afterburning thrust-vectoring turbofans developing 39,680lbs of thrust each.
Maximum Speed: 1,716 mph (2,761 kph; 1,491 knots)
Maximum Range: 2,485 miles (4,000 km)
Service Ceiling: 55,774 feet (17,000 meters; 10.56 miles)
Armament / Mission Payload
1 x 30mm Izhmash GSh-301 cannon
Base collection of Soviet/Russian air-to-air and air-to-surface missiles as needed across external or internal hardpoints (some sources include use of internal weapons bays).
R-77 (AA-12 "Adder") medium-range, radar-guided missiles.
R-73 (AA-11 "Archer") short-range, infrared-guided missiles.
K-37 long-range, radar-guided missiles
K-74 short-range infrared guided missiles
Conventional Drop Bombs
Global Operators / Customers
Model Variants (Including Prototypes)
Project 1.44 "Flatpack" - Project Designation; never entered production.
Project 1.42 "Foxglove" - Alternative Designation
MiG-MFI - Alternative Designation
MiG-35 - Early Designation; now since assigned to a further-developed MiG-29 Fulcrum model.