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SAM-25 Transport aircraft and coordination

SAM-25 Transport aircraft and coordination. First flight: 1943
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Technical specifications

DESIGNER Moskalev
COUNTRY Russia
TYPE
Transport aircraft and coordination
CREW 1
POWER-PLANT Two piston engines Μ-11F
Power, h.p. 1x140
DIMENSIONS  
Length, m 8,02
Height, m 3,86
Wing span, m 11,49
Wing area, m2 21,86
WEIGHT  
Maximum take-off, kg 1.280
Normal take-off, kg -
Empty aircraft, kg 845
Internal fuel, kg -
Warload, kg -
Payload, kg  
- passengers up to 7
PERFORMANCE  
Maximum speed, km/h 200
Max speed in low height, km/h 170
Cruising speed, km/h 168
Range, km 1.760
Combat range, km -
Service ceiling, m 4.860
Rate of climb, m/min -
Maximum overload, g -
ARMAMENT Doesn't have (defensive).