Hi! Sh-218. Perhaps radiators are located inner side of the twin boom.
http://aviadejavu.ru/Site/Arts/Art8692.htm
http://raigap.livejournal.com/154344.html
Design Start-1946
Flight of the first prototype-did not take place
Reason for completion-closing OKB No. 21
Length-13.88 m, Wingspan-16.43 m, Area of wing-45 square meters
Maximum-10500 kg mass, Normal mass-9000 kg, Empty mass-6693 kg, Mass of fuel-1200 kg
Max speed:-Earth-520 km/h, -At altitude of 2000 m-530 km/h
Climb-Height 5000 m for 5 min
Ceiling-6600 m
Range-1200 km
Run-up-520 m
Mileage-600 m
The engine is a piston-251 for the Power of 2000 hp (short to 2700 hp) with a coaxial rotor of AB-28 diameter of 3.6 m.
Crew-Two persons
borovik-san's chart is excellent.
http://www.secretprojects.co.uk/forum/index.php?action=dlattach;topic=9238.0;attach=96258;image
http://ourairports.biz/?p=6418
"The engine, mounted on the wing, was a Dobrynin VM-251 (in effect, half a VD-4, with three banks each of four cylinders) rated at 2,000hp. It drove an AV-28 contra-rotating propeller arranged for pusher propulsion, comprising two three-blade units each of 3.6m (11ft l0in) diameter."
VD-4 engine.
https://en.wikipedia.org/wiki/Dobrynin_VD-4K
https://www.google.co.jp/search?q=Alekseyev+I-218&source=lnms&tbm=isch&sa=X&ved=0ahUKEwihw6Pw1LXUAhVFNbwKHa_sC3QQ_AUIBigB&biw=1366&bih=617#imgrc=UPdWYWowmMj1bM:&spf=1497179894114