Shortround6
Major General
Thanks SR.
The "condesers" under the cylinder blocks may be heat exhchangers with liquid/vapour on one side and a cooling liquid on the other side. That is, maybe, 2 cooling circuits.
The book has one page on the He 100 system. 6 pages on the hot steam system and a 5 page 'chapter' on the 187B which was to use the system. It is not as detailed as it might sound becasue some 'chapters' are padded out with photo's that have no bearing on the subject. Like pictures of oil tank and a hydraulic valve block for landing gear in the cooling system chapter. BUT no mention is made of using ANY surface of the airplane as part of the cooling system. No pictures of such surface and of the few rather sketchy diagrams no 'surface' coolers seem to be involved, one sketch shows the motor, pumpe, dampf-Absch (? hard to read) and Kuhler.
There is a picture of a Bf 110 used to test the system with a rather large lumpy cowling with a lower intake that makes the Jumo 210 radiator look positively tiny.
I am convinced (short of photographic evidence to the contrary) that the FW 187 didn't use 'surface cooling" like the He 100.