Alekseyev I-21

Length
11.54 m
Flat Wing Span
12.25 m
Flat Wing Area
25 m²
Max Speed
950 km/h
Max Ceiling
13600 m
Number of Engines
2
Aircraft Engine
First Flight
1947-01-01
Number Built
3

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Aircraft Weight Variants

Aircraft
Alekseyev I-21

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All data (21 fields)
Name
Alekseyev I-21
Manufacturer
Alekseyev Design Bureau
Description
The Alekseyev I-21 was a Soviet twin-engined jet fighter, built in the late 1940s.
First Flight
1947-01-01
Service End
1947-01-01
Designer
Semyon Alekseyev
Length (m)
11.54
Cockpit Crew
1
Max Speed (km/h)
950
Max Ceiling (m)
13600
Rate of Climb (m/s)
27.78
Armament
2 × 23 mm Nudelman-Suranov NS-23 autocannon with 75 rounds per gun
National Origin
Soviet Union
Number Built
3
Powerplant Description
2 × Lyul'ka TR-1 axial-flow turbojet
Status
Prototype
Wikipedia Article (URL)
en.wikipedia.org/wiki/Alekseyev_I-21
Flat Wing Span (m)
12.25
Flat Wing Area (m²)
25
Aircraft Engine
Lyulka TR-1
Number of Engines
2