Technical data
Type RAF-11 RAF-11bis
Function Passenger, Trainer
Year 1938 1940
Crew 1-2?
Engines 2*300hp MG-31 2*330hp MG-31F
Length 10.86m 10.10m
Height ?m ?m
Wingspan 15.0m 15.0m
Wing area 30.0m2 30.0m2
Empty weight 2500kg 2097kg
Loaded weight 3720kg 3000kg
Wing Load (kg/m2) 109 100
Power load (kg/hp) 5.4 4.5
Maximum Speed at 0m 289km/h 294km/h
Cruising Speed at ?m 257km/h 254km/h
Landing Speed 110km/h 107km/h
Landing Roll 430m 22sec 335m 18sec
Takeoff Roll 440m 25sec 290m 18sec
Range 1000km 930km
Flight Endurance 4h 4h
Ceiling 4200m 4500m
Climb
1000m 4.1min 3.5min
2000m 8.3min 8.2min
3000m 14.7min 14.2min
4000m 35min 25.5min
Payload
Fuel+Oil 400+56kg 380+40kg
Cabin size LxWxH ?m3
Seats 6

RAF-11 and RAF-11bis by A.N.Rafaelants

48k b/w "History of aircraft construction in the USSR", Vol.1 p.572

Low-wing 2-engine wooden monoplane. Semi-monocoque fuselage provided room for 6 passengers. Retractable landing gear had main hydraulic and pneumatic emergency systems. Two-spar wing with fabric skin. Both aircraft were built at the GVF repair workshop.

RAF-11 was flown in 1938. Despite very clean shapes, aircraft was overweight and showed sluggish performance. Improved RAF-11bis was flight-tested in 1940. It was found successful and recomended for production as passenger for second class (??) airlines, trainer and 'transitional' (advanced trainer) aircraft.

Despite positive trials outcome, RAF-11 did not enter series production.


PredecessorsModifications
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ReferencesLinks
  • "History of aircraft construction in the USSR", Vol.1 p.573;
  • ....

  • Created July 7, 1999 Back to
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