Polikarpov I-185
1941
Back to the Virtual Aircraft Museum
  FIGHTERVirtual Aircraft Museum / USSR / Russia / Polikarpov  

Polikarpov I-185

Acceptance that the concept of the I-180 was outmoded coupled with the prospect of the availability of powerful 18-cylinder radial engines led the Polikarpov OKB to design the I-185 within an extraordinarily short period of time (25 January to 10 March 1940). Intended for the 1,750hp Shvetsov M-90 engine, the I-185 was of mixed construction, having a wooden monocoque fuselage mated with metal wings featuring automatic leadingedge slats a la Bf 109. Armament consisted of twin 12.7mm and twin 7.62mm guns, all fuselage-mounted. Development delays with the M-90 - which, by December 1940, was cleared only for restricted flight testing - resulted in dismantling of the first prototype unflown, this having been known as Samolet (Aircraft) R. A second prototype. Samolet RM, was completed with a Shvetsov M-81 18-cylinder two-row radial and a ducted propeller spinner. This was flown on 11 January 1941, but the M-81 was found to develop insufficient power and was replaced by the Shvetsov M-71 of 1,900hp in May 1941. A third prototype, Samolet I, was completed with a 14-cylinder Shvetsov M-82 engine rated at 1,330hp (later 1,400hp), the fuselage being lengthened for CG reasons from 7.68m to 8.10m, and fuselage-mounted armament being changed to three 20mm cannon. State Acceptance Tests were conducted successfully between 13 April and 5 July 1942. A fourth prototype reverted to the M-71 engine and this underwent operational evaluation on the Kalinin Front alongside Samolet I. A redesigned wing (of single- in place of two-spar construction) was featured by this aircraft, which was tested with both the four-machine gun and three-cannon armament arrangements. A pre-production prototype, the so-called I-185 Etalon (Standard), was flown on 10 June 1942. Regarded as the forerunner of the intended production derivative, the I-186, this standardised on the M-71 engine and three-cannon armament, and had a similarly lengthened fuselage to that of Samolet I. State Acceptance Testing was conducted between November 1942 and January 1943, the NIl VVS evaluation reports describing the I-185 Etalon as "superior to all contemporary fighters." In the event, it was found impracticable to manufacture the M-71 in large numbers and airframe production capacity was unavailable.

3-View 
Polikarpov I-185A three-view drawing (1278 x 930)


Specification 
 WEIGHTS
    Take-off weight3735 kg8234 lb
    Empty weight3130 kg6901 lb
 DIMENSIONS
    Wingspan9.80 m32 ft 2 in
    Length8.05 m26 ft 5 in
    Wing area15.53 m2167.16 sq ft
 PERFORMANCE
    Max. speed680 km/h423 mph

Comments 
rodney duffield, rod.rhonda(@)bigpond.com, 11.02.2008

are there any detailed plans including wing foils spar construction tail feather foil sections ect available ???Iam building a large scale version of this [i 185 m82] plane. I flew it on IL2 and it seemed like a nice aircraft

Do you have any comments about this aircraft ?

Name    E-mail


COMPANY
PROFILE



All the World's Rotorcraft


Virtual Aircraft Museum


All rhe World's Rotorcraft AVIATION TOP 100 - www.avitop.com Avitop.com