In 1937, the German Air Ministry – the Reichsluftfahrtministerium (RLM) – issued a specification for a single-engine reconnaissance aircraft with optimum visual characteristics.
The preferred contractors were Arado, but the request prompted the Focke-Wulf company to work up the alternative idea of the Focke-Wulf Fw 189, a twin-boom design with two smaller engines and a central crew gondola, while Blohm & Voss proposed something far more radical.
The proposal of chief designer Dr. Richard Vogt was the unique asymmetric BV 141.
The perspex-glazed crew gondola on the starboard side strongly resembled that found on the Fw 189, and housed the pilot, observer and rear gunner, while the fuselage on the port side led smoothly from the 746 kW (1,000 hp) Bramo 123 radial engine to a tail unit (which was symmetrical in the BV 141 V1 prototype).
It would seem that the displacement of lift vs weight, and thrust vs drag, would have induced tendencies to yaw and roll requiring continual trimming to control, but the aircraft proved very stable and maneuverable. Indeed, Dr. Vogt had calculated that the greater weight on one side of the aircraft could be cancelled out by the torque of the propeller.