Specifications and Performance
MiG-15UTI
Note:
These specifications refer to the Russian MiG-15UTI on which the
Lim-2 was based.
| Engine |
1
x 2 700kg (5 952lb) static thrust Klimov VK-1 turbojet |
|
Wing
Span
|
10.08m
|
33ft
0.75in
|
|
Length
|
10.04m
|
32ft
11.75in
|
|
Height
|
3.74m
|
12ft
1.5in
|
|
Wing
Area
|
20.6sq
m
|
221.7sq
ft
|
|
Weight
Empty
|
4
000kg
|
8
820lb
|
|
Weight
Loaded
|
5
400kg
|
11
905lb
|
|
Max
Speed
|
1
015km/h
|
630mph
|
|
Cruising
Speed
|
km/h
|
mph
|
|
Initial
Climb (MiG-15bis)
|
2
760m/min
|
9
050ft/min
|
|
Service
Ceiling
|
15
625m
|
47
980ft
|
|
Range
|
1
424km
|
885mile
|
|
