Mikoyan-Gurevich I-7

Length
16.93 m
Flat Wing Span
9.98 m
Flat Wing Area
31.9 m²
Max Speed
2300 km/h
Max Mach
1.18 Mach
Max Ceiling
19100 m
Number of Engines
1
First Flight
1957-04-22
Number Built
1
Maximum Take-Off Weight
11.54 t (paragliders: kg)
Maximum Range
1505 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Mikoyan-Gurevich I-7 11.54 1505

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All data (19 fields)
Name
Mikoyan-Gurevich I-7
Manufacturer
Mikoyan-Gurevich
Description
The Mikoyan-Gurevich I-7 was a development of the Mikoyan-Gurevich I-3 experimental fighter.
First Flight
1957-04-22
Designer
Mikoyan-Gurevich
Length (m)
16.93
Cockpit Crew
1
Max Speed (km/h)
2300
Max Ceiling (m)
19100
Armament
2 × 30 mm Nudelman-Rikhter NR-30 autocannon with 80 rpg; 4 × wing-root ZP-4 telescoping rotary rocket launchers in the wing roots rocket pods, each with 4x 57 mm S-5 rockets
Max Mach (Mach)
1.18
National Origin
Soviet Union
Number Built
1
Powerplant Description
1 × Lyulka AL-7F afterburning turbojet, 61.55 kN thrust each
Status
Prototype
Wikipedia Article (URL)
en.wikipedia.org/wiki/Mikoyan-Gurevich_I-7
Flat Wing Span (m)
9.98
Flat Wing Area (m²)
31.9
Number of Engines
1