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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.
 | A three-view drawing (1278 x 930) |
| WEIGHTS |
| Take-off weight | 3735 kg | 8234 lb |
| Empty weight | 3130 kg | 6901 lb |
| DIMENSIONS |
| Wingspan | 9.80 m | 32 ft 2 in |
| Length | 8.05 m | 26 ft 5 in |
| Wing area | 15.53 m2 | 167.16 sq ft |
| PERFORMANCE |
| Max. speed | 680 km/h | 423 mph |
| 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 |
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Do you have any comments about this aircraft ?
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