In 1937, Messerschmitt began '''
Projekt P. 1064'
, a study for a long-range reconnaissance aircraft, and took the design of the Bf 110 twin-engine heavy fighter (and derivative Bf 161 reconnaissance / Bf 162 light bomber projects) as its basis. The P. 1064 had a long, slim fuselage with two wing-mounted engines. The aircraft was planned from the outset as a record-breaking aircraft, but after becoming convinced that the aircraft was capable of taking the world long-distance flight record, the German Air Ministry (Reichsluftfahrtministerium'') approved the project and gave it the
airframe designation number of
8-261. The intended goal of the project was for an example of the aircraft to carry the
Olympic flame from
Garmisch-Partenkirchen, Germany (site of the
1936 Winter Olympics) to
Tokyo, Japan for the
1940 Summer Olympics in what would be a record-breaking nonstop flight The Me 261 incorporated a number of features which were highly advanced for its day. The single-
spar all-metal wing was designed to serve as a
fuel tank and its depth at the
wing root was only slightly less than the height of the fuselage. Power came from four
Daimler-Benz DB 601 engines, coupled together in pairs in a "power system" known as the DB 606, weighing 1.5 tonnes apiece and debuting in February 1937. The DB 606 "power systems" were originally developed for both the "single"-engined
Heinkel He 119 high-speed reconnaissance aircraft, and the
Heinkel He 177 strategic bomber, but the Me 261's design housed the DB 606 "power systems" in nacelles that afforded significantly better access for maintenance and ventilation of the "twinned" DB 601 component engines in each one, than
the Heinkel heavy bomber possessed. Each pair of engines drove a
variable-pitch propeller, intended to be a pair of
counter-rotating propellers (as the He 177A had used for its fourth prototype onwards) with each four-blade propeller driven through a gearbox shared between the "twinned" DB 601 engines forming the "power system", generating 2,700 PS (1,985 kW) each. The Me 261 had a
conventional landing gear with unusually large and bulky low-pressure tires, much like modern day aircraft
tundra tires, which prevented the aircraft from becoming bogged down on rough grass landing strips. The main gear's design appears to use main struts that rotated through 90° during their rearwards retraction sequence, with sizable main wheels resting atop the retracted struts (similar to those used on production examples of the contemporary
Junkers Ju 88). Even the Me 261's fully retractable tailwheel possessed a larger-than-average, low-pressure pneumatic tire. ==Operational history==