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

 

Compiled by Don Cameron