View source for Blohm & Voss BV 155

{{short description|German high-altitude prototype interceptor aircraft}}
{{More footnotes needed|date=January 2020}}
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{{Infobox aircraft
| name = BV 155
| image = BV 155 V2 43933212.jpg
| image_caption = Blohm & Voss BV 155 V2 [[prototype]]
| aircraft_type = High-altitude [[Interceptor aircraft|interceptor]]
| national_origin = [[Nazi Germany]]
| manufacturer = [[Blohm & Voss (aircraft)|Blohm & Voss]]
| designer = 
| first_flight = 1 September 1944
| number_built = 3
| unit cost = 
}}

The '''Blohm & Voss BV 155''' is a German high-altitude [[interceptor aircraft]] intended to be used by the [[Luftwaffe]] against raids by [[United States Army Air Forces|USAAF]] [[Boeing B-29 Superfortress]]es. Work started on the design as the Messerschmitt Me 155 in 1942, but the project went through a protracted development period and change of ownership, and prototypes were still under test and development when [[World War II]] ended.

==Background==
Performance estimates of the American [[B-29 Superfortress]] reached [[Germany|German]] command in early 1942. The bomber would cruise at an altitude at which no current German plane could operate effectively. To intercept it, the Luftwaffe would urgently need new aircraft. Work on such a high altitude fighter was begun by Messerschmitt, but in 1943 the project was passed to [[Blohm & Voss (aircraft)|Blohm & Voss]]. The result would be the Bv155 prototype that made its first test flight in September 1944.<ref name="Lepage p. 228">Lepage 2009, p. 228.</ref>

==Me 155==
The story of the BV 155 began at [[Messerschmitt]] in the spring of 1942. A requirement had arisen for a carrier-based single-seat [[Fighter aircraft|fighter]] to be based aboard the [[aircraft carrier]] {{Ship|German aircraft carrier|Graf Zeppelin||2}}, then under construction. In response, Messerschmitt proposed the '''Me 409''', later renamed '''Me 155'''. In the interest of economy and simplicity, it was to use as many [[Messerschmitt Bf 109]] components as possible, being basically a navalized version of the earlier Messerschmitt fighter.

The Me 155 was to be powered by a [[DB 605]]A-1 liquid-cooled engine of 1,475&nbsp;[[Horsepower#PS|PS]] (1,455&nbsp;hp, 1,085&nbsp;kW). The [[fuselage]] was more or less that of the standard Bf 109G, but with an entirely new wing. The [[Landing gear|undercarriage]] retracted inwards into wing wells, providing the wider track required for safe carrier landings. Standard naval equipment such as [[folding wing]]s, [[Aircraft catapult|catapult]] spools, and [[arrester gear]] were to be fitted. Proposed armament was an engine mounted 20&nbsp;mm [[MG 151 cannon]] and two 20&nbsp;mm MG 151 cannons and two 13&nbsp;mm (.51&nbsp;in) [[MG 131 machine gun]]s in the wings. It had an estimated maximum speed of 649&nbsp;km/h (403&nbsp;mph). Three variants were worked out, the Me 155A with one Junkers Jumo 213, the Me 155B powered by a [[DB 605#Variants|DB 628]], which was basically a [[DB 605]]A with a two-stage mechanical [[supercharger]] with an induction cooler, and the Me 155C with one DB 605A.

Detail design of the Me 155 was complete by September 1942. However, the numerous delays in the ''Graf Zeppelin'' seemed to indicate that the completion of the carrier would be at least two years away. Messerschmitt was told to shelve the Me 155 project for the indefinite future. Work on the ''Graf Zeppelin'' carrier was eventually abandoned.

===Me 155A===
In order that all of that work on the Me 155 project not go entirely to waste, Messerschmitt adapted its design in November 1942 to match a ''Luftwaffe'' requirement for a fast single seat bomber. A single 1,000&nbsp;kg (2,210&nbsp;lb) [[SC1000 bomb]] was to be carried. All of the carrier equipment and most of the armament was removed from the aircraft. Additional [[fuel tank]]s were provided and an elongated, non-retractable tailwheel was added to provide ground clearance for the large bomb. The proposal was designated Me 155A in late 1942.{{Sfn | Munson | 1978 | p =  33}}

===Me 155B===
By the end of 1942, the increasing number of USAAF bombing raids and intelligence coming in about the new American B-29 [[bomber]] led the ''Luftwaffe'' to revive development of the Me 155B. The engine was to be the DB 628, which was basically a DB 605A with a two-stage mechanical supercharger with an induction cooler. A [[Cabin pressurization|pressurized cabin]] was to be provided. It was estimated that a service ceiling of 14,097&nbsp;m (46,250&nbsp;ft) could be attained.

A converted Bf 109G adapted to take the DB 628 engine flew in May 1942 and attained an altitude of 15,500&nbsp;m (50,850&nbsp;ft). However, the ''Technische Amt'' concluded that a [[DB 603]]A engine with an exhaust-driven [[Twincharger|turbosupercharger]] was more promising. The DB 603A provided 1,201&nbsp;kW (1,610&nbsp;hp) for takeoff and 1,081&nbsp;kW (1,450&nbsp;hp) at 15,000&nbsp;m (49,210&nbsp;ft). This engine change required that the fuselage be elongated in order to house the turbosupercharger aft of the pressure cabin. Exhaust gases were carried to the turbosupercharger via external ducts. Air was drawn in through via a ventral trough aft of the wing. Standard Bf 109G wings were to be fitted outboard of a new, long-[[Wingspan|span]], untapered wing center section. Other parts were scavenged from existing Messerschmitt designs – the vertical tail was from the Me 209, and the horizontal tail and the undercarriage were taken from the Bf 109G. The resulting revision of the Me 155B was designated '''P.1091''' by Messerschmitt.

In August 1943, the RLM realised that Messerschmitt was over-committed and transferred the design work to Blohm & Voss. The design team there came to the conclusion that the existing Messerschmitt design had too many weaknesses and a complete redesign would be necessary.<ref name="Amtmann63-4">Hans Amtmann; ''The Vanishing Paperclips'', Monogram, 1988, Pages 63-64.</ref>{{Sfn | Munson | 1978 | p =  33}}

==BV 155==
In September 1943, an order for five [[prototype]]s was placed. Blohm & Voss accepted the order only on condition they had complete design freedom and were not bound by Messerschmitt's work to date.<ref name="Amtmann63-4" /> The redesign was named the '''BV 155'''. B&V gave it a new [[laminar flow]] wing and tail unit, landing gear from the [[Junkers Ju 87|Ju 87]] and many other parts of the plane. Further wind tunnel testing showed that there was a serious problem with the overwing radiators, at high [[angle of attack|angles of attack]] the wing "blanked" them from the airflow and cooling would suffer. Work moved to a revised B model.

The first prototype, BV 155 V1, took off for its maiden flight on 1 September 1944. Tests with the V1 showed that the outboard radiators provided inadequate cooling, especially at high angle of attack. The intakes on the next prototype were enlarged and underslung beneath the wing rather than placed over it. However, the enlarged radiators changed the aircraft's center of gravity which required moving the pressurized cockpit forward. The Blohm & Voss team took this opportunity to replace the original Bf 109G canopy with an aft-sliding all-round vision canopy, and the rear fuselage decking was cut down. This in turn required that a larger rudder be fitted. The ventral radiator bath was also enlarged.

With these changes, the BV 155 V2 flew on 8 February 1945. Blohm & Voss was still not satisfied with the design, and before the V2 began its flight trials they proposed that the engine be switched to the DB 603U having the larger mechanically driven supercharger of the DB 603E. The DB 603U promised a power of 1,238&nbsp;kW (1,660&nbsp;hp) for takeoff and 1,066&nbsp;kW (1,430&nbsp;hp) at 14,935&nbsp;m (49,000&nbsp;ft). The ventral turbosupercharger was retained. The Technische Amt decided to accept this proposal, and abandoned all work on the BV 155B in favor of the revised design, which was designated BV 155C.

The BV 155 V2 was damaged beyond repair during a bad landing. It was to be replaced in the test program by the BV 155 V3. The BV 155 V3 differed from the V2 in having the DB 603U intended for the BV 155C. However, the engine [[cowling]] and turbosupercharger were unchanged.

Various armament schemes for the BV 155B were proposed. One proposal had an engine-mounted (or ''Motorkanone'') 30&nbsp;mm (1.18&nbsp;in) [[MK 108 cannon]] and two 20&nbsp;mm MG 151/20 cannons. Another had a ''Motorkanone''-mount 30&nbsp;mm (1.18&nbsp;in) [[MK 103 cannon]] and two wing-mounted 20&nbsp;mm MG 151 cannons. Estimated maximum speed was 650&nbsp;km/h (400&nbsp;mph) at 12,000&nbsp;m (39,370&nbsp;ft) and 690&nbsp;km/h (430&nbsp;mph) at 15,999&nbsp;m (52,490&nbsp;ft). Service ceiling was to be 16,950&nbsp;m (55,610&nbsp;ft). Empty weight was 4,869&nbsp;kg (10,734&nbsp;lb). Normal loaded weight ranged from 5,126-5,488&nbsp;kg (11,300-12,100&nbsp;lb), depending on the armament provided.

According to the Pegasus Models Kit No. 5002 information sheet, V1 and V2 were both provided to the RAF after the war. V1 was flight-tested until it was written off. The fate of V3 is not known, except that it was left half-finished by the end of the war. V2 is in storage at the Smithsonian's [[Paul E. Garber Preservation, Restoration, and Storage Facility|National Air And Space Museum's storage facility]].

===BV 155C Project===
In parallel with the prototype development, Blohm & Voss had been working on additional changes under ''Project 205''. P.205 replaced the underwing radiators with an annular one around the front of the engine, a design feature commonly found on a number of German designs. With the wings now free of clutter, they were considerably simpler and were reduced in span. This also had the side effect of reducing the track, which would later prove to be a welcome change. The new design would be simpler, lighter and faster, and plans were made to make it the standard version of the aircraft. During the October re-evaluation, it was agreed that V1 and V2 would be completed as B models, while the V3 would be the prototype for the BV 155C.{{Sfn | Munson | 1978 | p =  33}}

The BV 155C was to be significantly different in appearance from the BV 155B. The clumsy wing-mounted radiators of the BV 155B were eliminated, and the main landing gear leg attachment points were moved inboard to retract inwards. Cooling was provided by an annular frontal radiator as in the [[Focke-Wulf Ta 152]]. Large circular intakes were attached to the fuselage sides above the wing roots. 30 were ordered but none were built. The V3 was 75% compelete when it was captured. Intended armament for the 155C was two wing-mounted 20mm [[MG 151/20]] cannons and a 30mm MK 108 cannon firing through the spinner.{{Sfn | Munson | 1978 | p =  33}}

==Specifications (BV 155B)==
{{Aircraft specs
|ref=<ref name="Greenaottr">Green 2010, pp. 148–152.</ref>
|prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show -->
<!--
        General characteristics
-->
|genhide=

|crew=1
|length m=12
|span m=20.5
|height m=3
|wing area sqm=39
|empty weight kg=4,870
|gross weight kg=5,520
|gross weight note=Proposal A<br />
::::{{convert|5,125|kg|lb|abbr=on|0}} Proposal B
::::{{convert|5,100|kg|lb|abbr=on|0}} Proposal C
::::{{convert|5,440|kg|lb|abbr=on|0}} Proposal D
|max takeoff weight kg=6,020
|fuel capacity={{convert|1,200|L|impgal|abbr=on|0}}
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=[[Daimler-Benz DB 603A]]
|eng1 type=inverted V-12 liquid-cooled piston engine with [[TKL 15]] turbo-charger
|eng1 kw=1,200
|eng1 note=for take-off<br />
::::{{convert|1,200|kW|hp|abbr=on|0}} at {{convert|10,000|m|ft|abbr=on}}
::::{{convert|1,081|kW|hp|abbr=on|0}} at {{convert|15,000|m|ft|abbr=on}}

|prop blade number=4
|prop name=constant speed paddle bladed propeller
<!--
        Performance
-->
|max speed kmh=420
|max speed note=at sea level<br />
::::{{convert|520|km/h|mph|abbr=on|0}} at {{convert|6,000|m|ft|abbr=on}}
::::{{convert|600|km/h|mph|abbr=on|0}} at {{convert|10,000|m|ft|abbr=on}}
::::{{convert|650|km/h|mph|abbr=on|0}} at {{convert|12,000|m|ft|abbr=on}}
::::{{convert|690|km/h|mph|abbr=on|0}} at {{convert|16,000|m|ft|abbr=on}}
|range km=460
|range note=at maximum continuous power with {{convert|595|L|impgal|abbr=on|0}} of fuel at sea level<br />
::::{{convert|560|km|mi|abbr=on|0}} with {{convert|595|L|impgal|abbr=on|0}} of fuel at {{convert|10,000|m|ft|abbr=on}}
::::{{convert|590|km|mi|abbr=on|0}} with {{convert|595|L|impgal|abbr=on|0}} of fuel at {{convert|16,000|m|ft|abbr=on}}
::::{{convert|1,080|km|mi|abbr=on|0}} with {{convert|1,200|L|impgal|abbr=on|0}} of fuel at sea level
::::{{convert|1,350|km|mi|abbr=on|0}} with {{convert|1,200|L|impgal|abbr=on|0}} of fuel at {{convert|10,000|m|ft|abbr=on}}
::::{{convert|1,440|km|mi|abbr=on|0}} with {{convert|1,200|L|impgal|abbr=on|0}} of fuel at {{convert|16,000|m|ft|abbr=on}}
|ceiling m=16,950
|ceiling note=service ceiling<br />
*'''Maximum ceiling''' {{convert|17,100|m|ft|abbr=on}}
|climb rate ms=11.5
|climb rate note=initial<br />
::::{{convert|3.92|m/s|ft/s|abbr=on|0}} at {{convert|16,000|m|ft|abbr=on}}
|time to altitude= {{convert|16,000|m|ft|abbr=on}} in 29 minutes
<!--
        Armament
-->
|guns=<br />
::'''Proposal A'''
:::* 1 × {{convert|30|mm|in|abbr=on|3}} [[MK 108 cannon]] as an engine mounted ''Motorkanone'' firing through the propeller shaft{{Citation needed|date=December 2011}}
:::* 2 × 20 mm [[MG 151 cannon|MG 151/20 cannon]]
::'''Proposal B'''
:::* 1 × {{convert|30|mm|in|abbr=on|3}} [[MK 103 cannon]] as an engine mounted ''Motorkanone'' firing through the propeller shaft with 60 rounds
:::* 2 × {{convert|15|mm|in|abbr=on|3}} [[MG 151 cannon]] with 200 rpg
::'''Proposal C'''
:::* 3 × {{convert|30|mm|in|abbr=on|3}} [[MK 108 cannon]] with 60 rpg.
::'''Proposal D'''
:::* 3 × {{convert|30|mm|in|abbr=on|3}} [[MK 103 cannon]] with 60 rpg (two mounted in under-wing fairings).
}}

==See also==
{{aircontent
<!-- other related articles that have not already linked and do not fit the specific entries below: -->
|see also=

<!-- "Related development", developed into or from this design: -->
|related=

<!-- "Aircraft of comparable role, configuration and era" as this design: -->
|similar aircraft=
* [[Fisher P-75 Eagle]]
* [[Focke-Wulf Ta 152]]
* [[Kawasaki Ki-64]]
* [[Nakajima Ki-87]]
* [[Republic XP-72]]
* [[Westland Welkin]]

<!-- "Related lists", relevant lists where this design appears -->
|lists=
* [[List of military aircraft of Germany]]

<!-- See [[WP:Air/PC]] for more explanation of these fields. -->
}}

==References== 
{{Reflist}}

==Sources==
* Green, William. ''Aircraft of the Third Reich'' (1st ed.). London: Aerospace Publishing Limited, 2010. {{ISBN|978-1-900732-06-2}}.
* Green, William. ''Warplanes of the Second World War, Volume One: Fighters''. London: Macdonald & Co.(Publishers) Ltd., 10th impression 1972, p.&nbsp;80-82. {{ISBN|0-356-01445-2}}.
* Green, William. ''Warplanes of the Third Reich''. London: Macdonald and Jane's Publishers Ltd., 4th impression 1979, p.&nbsp;88-91. {{ISBN|0-356-02382-6}}.
* Hitchcock, Thomas H. ''Blohm & Voss 155 (Monogram Close-Up 20)''. Sturbridge, Massachusetts: Monogram Aviation Publications, 1990. {{ISBN|0-914144-20-0}}.
* Lepage, Jean-Denis G.G.. ''Aircraft of the Luftwaffe, 1935-1945: An Illustrated Guide''. Jefferson, North Carolina: McFarland & Company, 2009. {{ISBN|978-0-7864-3937-9}}.
* {{cite book |last = Munson |first = Kenneth |title = German Aircraft Of World War 2 in colour |location = Poole, UK |publisher = Blandford Press |year = 1978 |isbn = 0-7137-0860-3}}
*{{cite book |last1=Sharp |first1=Dan |title=Blohn & Voss BV155 |date=2019 |publisher=Tempest Books |location=Horncastle, UK |isbn=978-1-911658-32-0}}
* Smith J. Richard and Anthony L. Kay. ''German Aircraft of the Second World War''. London: Putnam & Company Ltd., 1978, p.&nbsp;88-91. {{ISBN|0-370-00024-2}}.
* Wood, Tony and Bill Gunston. ''Hitler's Luftwaffe: A pictorial history and technical encyclopedia of Hitler's air power in World War II''. London: Salamander Books Ltd., 1977, p.&nbsp;136. {{ISBN|0-86101-005-1}}.

==External links==
{{commons category|Blohm & Voss BV 155}}
* https://web.archive.org/web/20060517014448/http://www.csd.uwo.ca/~pettypi/elevon/baugher_other/bv155.html#RTFToC2
* https://web.archive.org/web/20060511171223/http://luftfahrtmuseum.com/htmd/dtf/bv155.htm (in German)

{{Bf 109 family}}
{{Hamburger Flugzeugbau aircraft}}
{{Messerschmitt aircraft}}
{{RLM aircraft designations}}
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{{DEFAULTSORT:Blohm and Voss Bv 155}}
[[Category:1940s German fighter aircraft]]
[[Category:Single-engined tractor aircraft]]
[[Category:Low-wing aircraft]]
[[Category:Blohm & Voss aircraft|BV 155]]
[[Category:Aircraft first flown in 1944]]
[[Category:Aircraft with retractable conventional landing gear]]
[[Category:Single-engined piston aircraft]]