| After completion by the TsAGI of full-scale wind tunnel
testing of the I-210 alias IKh, the OKB redesigned the
junction between the engine cowling and the fuselage.
It moved the pilot's cockpit aft, enlarged the vertical tail
surfaces, redesigned the engine cowling and repositioned
the oil cooler intakes in the wing roots. The
undercarriage was redesigned, power was provided by
a Shvetsov M-82F radial engine of 1700hp and armament
was restricted to a pair of wing-mounted 20mm
ShVAK cannon. Only the outer wing panels of the
MiG-3 remained and slots were applied to these. This
thoroughgoing redesign of the I-210 was referred to as
the I-211, or Ye, a pre-series batch of 10 aircraft being
laid down of which the first flew in August 1942. Factory
testing was completed within one month, the results
being highly successful, but no manufacturing
capacity was available for production, and all aerodynamic
data and information on the slots were passed
to the Lavochkin OKB as a result of a ministerial request.
| A three-view drawing (1667 x 1150) |
WEIGHTS |
Take-off weight | 3100 kg | 6834 lb |
Empty weight | 2528 kg | 5573 lb |
DIMENSIONS |
Wingspan | 10.20 m | 33 ft 6 in |
Length | 7.95 m | 26 ft 1 in |
Height | 3.63 m | 12 ft 11 in |
Wing area | 17.44 m2 | 187.72 sq ft |
PERFORMANCE |
Max. speed | 670 km/h | 416 mph |
Range | 1140 km | 708 miles |
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