Technical data
Type MR-3bis
Function Naval Recce
Year 1931
Crew 2
Engines 1*500/680hp M-17
Length 11.4m
Wingspan 15.6m
Wing area 53.0m2
Empty weight 2050kg
Loaded weight 3100kg
Wing Load (kg/m2) 59.0
Power load (kg/hp) 6.2
Speed at 0m 190km/h
Landing Speed 85km/h
Landing Roll 22sec
Takeoff Roll 35sec
Range 720km
Flight Endurance 4h
Ceiling 4000m
Armament
Guns 1...2mg?
Bombs ?

MR-3bis, MR-5bis, Product '0' by I.V.Chetverikov (OPO-4)

60k b/w photo "History of aircraft construction in the USSR", Vol.1 p.403

Biplane flying boat, development of the MR-3. Hull was redesigned (new shape, wooden construction). Aircraft was ready in June 30, 1931. Takeoff shortcomings were cured without changes in flight performance.

There was another variant of the hull built for special high speed monoplane design (MR-5, MR-5bis). But more advanced project MBR-2 was on its final stage, and MR-5bis was not finished.

PredecessorsModifications

MR-3
None. Dead End.

ReferencesLinks
  • "History of aircraft construction in the USSR", Vol.1 p.404;
  • None?

    Created July 29, 1998 Back to
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