Mikoyan-Gurevich I-3

Length
15.78 m
Flat Wing Span
8.98 m
Flat Wing Area
30 m²
Max Speed
1960 km/h
Max Mach
1.59 Mach
Max Ceiling
18800 m
Number of Engines
1
Aircraft Engine
First Flight
1956-01-01
Number Built
1
Maximum Take-Off Weight
10.028 t (paragliders: kg)
Maximum Range
1290 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Mikoyan-Gurevich I-3 10.028 1290

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All data (19 fields)
Name
Mikoyan-Gurevich I-3
Manufacturer
Mikoyan-Gurevich
Description
The Mikoyan-Gurevich I-3 was the first of three interrelated fighter prototype programs developed by the Mikoyan-Gurevich design bureau in the Soviet Union in the mid/late 1950s – starting with the I-3, continuing with the I-7 and finally evolving into the I-75.
First Flight
1956-01-01
Designer
Mikoyan-Gurevich
Length (m)
15.78
Cockpit Crew
1
Max Speed (km/h)
1960
Max Ceiling (m)
18800
Armament
2 × 30 mm Nudelman-Rikhter NR-30 autocannon
Max Mach (Mach)
1.59
National Origin
Soviet Union
Number Built
1
Powerplant Description
1 × Klimov VK-3 afterburning turbojet engine, 82.4 kN thrust each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Mikoyan-Gurevich_I-3
Flat Wing Span (m)
8.98
Flat Wing Area (m²)
30
Aircraft Engine
Klimov VK-3
Number of Engines
1