La-5UTI Training aircraft. First flight: 1944

 


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TECHNICAL SPECIFICATIONS

DESIGNER OKB Lavochkin
COUNTRY Russia
TYPE Training aircraft
CREW 2
POWER-PLANT One reciprocating motor M-82F
Thrust, h.p 1 x 1.330
DIMENSIONS  
Length, m 8,67
Height, m 2,54
Wing span, m 9,80
Wing area, m2 17,50
WEIGHT  
Normal take-off, kg 3.210
Empty aircraft, kg 2.789
Maximum take-off, kg -
Internal fuel, kg -
PERFORMANCE  
Maximum speed, km/h 600
Cruising speed, km/h -
Max speed in low height, km/h 552
Rate of climb, m/min 887
Service ceiling, m 10.000
Range, km 720
Combat range, km -
ARMAMENT One 20 mm cannon ShVAK