не бьет с этим:
"BMW 801 Q (TU)
14 cylinders in two rows, radial engine with 1 stage 2 speeds compressor, Air-cooled (12-bladed-fan assisted), using direct injection and C3 (96-100 % octane) fuel. This engine is a hybrid engine using parts of the BMW801 D and F/E.
The assembly chart gives use the part number for the TU: 9-8801 U1. The captured A8 from September 44 (PR0 AIR 40/151) confirms that the part number 9-8801 U1 is associated to the BMW 801 Q."
"BMW 801 S (TS)
14 cylinders in two rows, radial engine with 1 stage 2 speeds compressor, Air-cooled (12 -bladed-fan assisted), using direct injection and C3 (96-100 % octane) fuel. This is another hybrid between the BMW801 D and the E. Erhöhte Notleistung device serialised in January 45.
This engine was used on the A9, F9 and G9
Part number: 9-8801 S1"
"BMW 801 E (TH)
14 cylinders in two rows, radial engine with 1 stage 2 speeds compressor, Air-cooled (12-bladed-fan assisted), using direct injection and C3 (96-100 % octane) fuel.
Erhöhte Notleistung device planed to be serialised in March 45.
Part number: 9-8801 H1"
"BMW801 Q (TU) no data so far probably close to the TS under 6000 m and close to the D.
the bleeding of the airline was serialised
BMW 801 S (TS)
2000 ps (1.65 ATA) around 2200 with the bleeding of the airline (alledgedly installed in january 45)
the Q and the S are basically d engines with F components.
Installing MW50, according to a document from jan 45, was difficult on the D,S,Q. but easier on the E/F.
BMW 801 E (TH)
2000 ps (1.65 ATA) almost all new components.
the bledding of the airline was to be serialised in march 45. Mw50 was tested and possible to install)"
P.S. 801 Е построили около 60 штук. с тем же успехом можно сказать что у нас в серии были М-71 и М-71Ф...![]()






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