SM-6 Experimental Ekranoplans. First flight: 1972

 


 Technical specifications      Photos      Video

 

 

 

 

 

 

 


TECHNICAL SPECIFICATIONS

Maximum take-off, kg 26.500
Payload, kg -
Length, m 31,0
Height, m 7,9
Wing span, m 14,8
Wing area, m2 73,8
Maximum speed, km/h 350
Power-plant An Ivchenko AI-25 turboprop engine driving a four-bladed AV-68 propeller for cruise, mounted atop the fin, and two booster-cruise turbojet engines in the nose (AI-20).
Thrust, kgf -
Service ceiling, m -
Range, km 700
Passengers -
Crew -