Petrus said:
Very interesting!
BTW, do you have any idea what engine/engines the I-218-2 (i.e. the jet-powered variant) had? I would like to know its dimensions and other data, including its planned armament. Does anybody know anything on that?
Best regards,
Piotr
Sorry Piotr, its lack of attentiveness (noticed only now) :-[
"218" - Span -16,43m, length-13,88m, wing area-45,0m2, take-off weight of 9000kg, max. speed- 465km /h, range-1200km, engine-VD-251 (M-250) / Dobrynin, propeller AV-28 the diameter of 3,6 m.
"218-II" - Span -17,4m, length-16,5m, wing area-50,0m2, take-off weight 13000kg, max. speed-735km /h, range-1200km, engine -TR-3/Lyul 'ka or VK-1/Klimov
"218-III" - scale-18,4m, length-17,0m, wing area-55,0m2, take-off weight 12000kg, max. speed-504km / h, range-1300km, engine -M-250/Dobrynin
Armament underneath the fuselage could stoop down to 25-30 degrees.
Planned or 4xNR-23 (to 150 rounds per gun), or 2xN-37 (40), or 2xN-57 (30)
To defend the back-2x20mm gun with remote control ( "218" on the booms), ( "218-III" on the wing) (120)
In the fore part of the booms were placed on three rocket guns ORO-132, ( "218-II", "218-III" under the wing)
In the bomb bay could hang 6x100kg bombs or smaller in the appropriate quantities.
Under the fuselage provided accommodation bomb or torpedo weight to 1500kg. (in overload)