The origins of the Blohm & Voss Bv 155 lay in a meeting held at the Messerschmitt’s Augsburg plant in May 1942 to discuss the “Special High Altitude Fighter”. Both Messerschmitt and Fock-Wulf expressed interest in developing a special high altitude fighter, Messerschmitt had already done some design work on a related project. Messerschmitt’s preliminary study, known as the Bf 109 ST, had been allocated the official RLM 8-series aircraft designation Me 155. The number 155 had previously been assigned to the Klemm firm but since it had not taken up the number the RLM reassigned it to Messerschmitt. At the same time, numbers 152, 153 and 154, which had also been allocated to Klemm but not used, were re-assigned to Focke-WuIf. The original Me 109 ST was advanced in three variants; A, B & C (version A) called for a carrier/aircraft fitted with the DB 605, while (version B) called for a similar fighter powered by the high altitude DB 628. In order to relieve his already over committed design bureau and to speed development, Messerschmitt decided to transfer the Me 155B to Paris. Due to various problems work progressed only slowly throughout the remainder of 1942. By early 1943 things were starting to go wrong with the project. Fock-Wulf were progressing well with their Ta 152, little had been achieved with the Me 155B. During the first half of 1943, Messerschmitt’s design engineers had evolved basic parameters of an (extreme high altitude fighter) design study under the company designation Me P1091. By mid 1943 the Messerschmitt people were pursuing the Me 209H in competition with the Ta 152H and turning there Me P1091 in to the Me 155B.
Development passed to Blohm & Voss as the Bv 155. The V1, V2 and V3 prototypes were outwardly very different, mainly by relocation of the radiators. The final Bv 155C had the cooling systems under the nose. A contract for 30 production aircraft was issued in the finals days of WWII. Never flown.
The V1 prototype first flew on 01 September 1944, and V2 in February 1945. Three prototypes were built.

Engine: Daimler Benz DB 603A,1610 hp with turbocompressor TKL 15 (1,450 hp at 49,210 ft. (15,000m))
Propeller: metal three-bladed variable pitch
Wingspan: 20,30 m / 67 ft. 3 in
Length: 11,90 m / 39 ft 4 1/2 in
Height: 2,98 m / 9 ft 9 1/2 in
Wing area: 39,00 sq.m
Empty weight: 4868 kg / 10,716 lb
Maximum weight: 13,262 lb. (6016 kg)
Wing loading: 141,025 Kg/sq.m
Power loading: 3,105 Kg/hp
Max speed: 690 Kmh
Ceiling: 16950 m
Range: 1440 km
Armament: 1 x 30 mm MK 108, 2 x 20 mm MG 151/20

Resulting from a 1937 requirement for a short-range reconnaissance plane with a single engine and accommodation for a crew of three, Richard Vogt, the technical director of Blohm und Voss’s aircraft subsidiary, Ham¬burger Flugzeugbau, proposed that an official RLM requirement could best be met by an asymmetric design. The result was the company financed Ha 141 0, flown in Feb¬ruary 1938 with Major General Ernest Udet at the controls. An unorthodox machine with an extensively glazed crew nacelle offset to starboard of the centerline and the 865-hp (645-kW) BMW 132N radial engine to port at the front of the boom supporting the tail unit. A perspex-glazed crew gondola on the starboard side housed the pilot, observer and rear gunner, while the fuselage on the port side led smoothly from the engine to a tail unit.

The engine was a conventional radial piston powered machine spinning a three-bladed propeller system. The engine of choice became a single BMW 801A 14-cylinder radial of 1,560 horsepower providing for a 272mph maximum speed, a 1,181 mile range and a 31,810 foot service ceiling. The later pre-series Bv 141s would make use of only a single tail system, hence its asymmetrical arrangement. Despite this appearance, the weight of the aircraft was spread out quite well when in flight, relating to the Bv 141s good handling characteristics.

It proved to be quite successful, so much so that an order was placed for three planes including the original, since that one was built with private funds. The original BV-141-V and A models had a conventional stabilizer.

The aircraft’s design prompted a mixed response from the RLM and had no impact on their decision to build the Fw 189. Indeed, an urgent need for BMW 801 engines for use in the Fw 190 fighter aircraft further reduced any chance that the BV 141 would see production. Though the RLM officials remained uncertain of its potential they awarded a contract for further for five Bv 141A developed versions with 960L hp BMW 132N engine and armament of two fixed and two rear movable 7.92 mm (0.312¬in) MG 17 and four 50 kg (110 lb) bombs. Lengthy trials in 1939 40 were favourable, but the RLM claimed that the oddity was under-powered as an excuse to avoid large scale orders.

The German air ministry preferred the competing Focke-Wulf Fw 189, but the manufacturer’s enterprise in building three prototypes, the last two somewhat larger than the first, paid off in an order for five pre-production By l4lAs. These were evaluated up to April 1940, but no production was ordered even of the more powerful Bv 141B.

Vogt had anticipated this and in January 1941 flew the first completely redesigned Bv 141B with 1560 hp BMW 801 and larger airframe of different shape, including an asymmetric tailplane, first tested on the V2 prototype, designed to improve the rear gunner’s field of fire and which had resulted in no noticeable deterioration in handling qualities.

Only five B series aircraft were built, making 13 of all versions. No 10 was used operationally in the autumn of 1941, but this unique aircraft was eventually dropped as the twin boom Fw 189 was an adequate tactical reconnaissance aircraft and the Blohm und Voss shops were needed to help make the Fw 200C Condor after an air raid had damaged the Focke Wulf factory complex at Bremen.

All further development was cancelled in 1942.

Some 38 Bv 141 examples were known to have been produced though none survive today. Several were recovered by the Allies. In all, there were three V-series prototypes designated as V1, V2 and V3. The pre-series models numbered five examples under the Bv 141 A-0 branding and became V4 through V8. These were followed by the revised Bv 141 B-0 pre-series models from V9 through V18. There were eight Bv 141 B-1 series models thereafter.

The Ilmavoimat / Maavoimat / VL team evaluated this aircraft and conducted a series of test flights over April/May 1938. The performance was found to be good and the observation visibility excellent although STOL capability was lacking. Overall though, the design was rather too radical for the Finns and while it remained in consideration, it was as a “possibility” rather than up for firm consideration.

Bv 141A
five pre-production aircraft
Engine: 1,000-hp/746-kW BMW-Bramo 323
Wing span: 50 ft 8.25 in/15.45m

Bv 141B
three-seat short-range reconnaissance plane.
Engines: one 1,560-hp (1,163-kW) BMW 801A radial piston
Maximum speed: 230 mph (370 km/h) at sea level
Service ceiling: 32,810 ft (10,000 m)
Range: 746 miles (1,200 km).
Empty Weight: 10,362 lb (4,700 kg)
Maximum take-offweight: 13,448 lb (6,100 kg).
Span: 57 ft 3.5 in (17.46 m)
Length: 45 ft 9.25 in (13.95 m)
Height: 11 ft 9.25 in (3.60 m)
Wing area: 570.51 sq ft (53.00 sq.m)
Rate-of-Climb: 1,860ft/min (567m/min)
Crew: 3
Armament: two fixed MG 17 and two trainable MG 15 0.312-in (7.92-mm) machine guns, and four 110-lb (50-kg) bombs.