Mikoyan MiG-29

Length
17.32 m
Flat Wing Span
11.36 m
Height
4.73 m
Flat Wing Area
38 m²
Max Speed
2450 km/h
Max Mach
2.3 Mach
Max Ceiling
18000 m
Number of Engines
2
Aircraft Engine
First Flight
1977-10-06
Entry Into service
1983-08-01
Number Built
1600
Maximum Take-Off Weight
18 t (paragliders: kg)
Maximum Range
1430 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Mikoyan MiG-29 18 1430

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All data (28 fields)
Name
Mikoyan MiG-29
Manufacturer
Mikoyan-Gurevich
Description
The Mikoyan MiG-29 (; NATO reporting name: Fulcrum) is a twin-engine fighter aircraft designed in the Soviet Union.
ICAO Code
MG29
First Flight
1977-10-06
Entry Into service
1983-08-01
Production End
2019-01-01
Designer
Mikoyan-Gurevich
Type
Air superiority fighter, multirole fighter
Length (m)
17.32
Height (m)
4.73
Cockpit Crew
1
Max Speed (km/h)
2450
Max Ceiling (m)
18000
Rate of Climb (m/s)
330
Armament
1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon. Originally held 150 rounds, reduced to 100 on later variants.; 7 × hardpoints (6 × underwing, 1 × fuselage)
Max Mach (Mach)
2.3
National Origin
Soviet Union
Number Built
1600
Powerplant Description
2 × Klimov RD-33 afterburning turbofan engines, 49.42 kN thrust each
Primary Users
Russian Aerospace Forces, Indian Air Force, Algerian Air Force, Ukrainian Air Force
Status
In service
Wikipedia Article (URL)
en.wikipedia.org/wiki/Mikoyan_MiG-29
Flat Wing Span (m)
11.36
Flat Wing Area (m²)
38
Wake Category
M
Aircraft Engine
Klimov RD-33
Number of Engines
2