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((Redirect|Ta-183|the isotope of tantalum (Ta-183 or <sup>183</sup>Ta)|Tantalum-183))
((Short description|Jet powered interceptor concept aircraft))
((More citations needed|date=September 2010))
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]].  Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{|((Infobox aircraft begin
| name = Ta 183 ''Huckebein''
| image = File:Ta183-1.jpg
| caption = Wind tunnel model
))((Infobox aircraft type
| type = Fighter/Interceptor
| manufacturer = [[Focke-Wulf]]
| designer = 
| first flight = 
| introduced = 
| retired = 
| produced = 
| number built = None completed
| status = Terminated by the end of the war
| unit cost = 
| primary user = [[Luftwaffe]]
| more users = 
| developed from = 
| variants with their own articles = 
| developed into = [[Focke-Wulf Volksjäger]],<br>[[Focke-Wulf Super Lorin]]<br>[[FMA IAe 33 Pulqui II]]
))
|}

The '''Focke-Wulf Ta 183 ''Huckebein''''' was a design for a jet-powered [[fighter aircraft]] intended as the successor to the [[Messerschmitt Me 262]] and other [[day fighter]]s in [[Luftwaffe]] service during [[World War II]]. It had been developed only to the extent of [[wind tunnel]] models when the war ended, but the basic design was further developed postwar in Argentina as the [[FMA IAe 33 Pulqui II]]. The name ''Huckebein'' is a reference to a trouble-making [[raven]] (''Hans Huckebein der Unglücksrabe'') from an illustrated story in 1867 by [[Wilhelm Busch]].<ref>[http://gutenberg.spiegel.de/buch/hans-huckebein-6042/1 "Hans Huckebein."] ''Spiegel online''. Retrieved: 5 April 2015.</ref>

==Development==
In early 1944, the [[Reich Air Ministry]] (RLM, for ''Reichsluftfahrtministerium'') became aware of [[Allies of World War II|Allied]] jet developments, and were particularly concerned that they might have to face the [[Gloster Meteor]] over the continent. In response, they instituted the [[Fighter Emergency Program|Emergency Fighter Program]] which took effect on July 3, 1944, ending production of most [[bomber]] and multi-role aircraft in favour of fighters, especially jet fighters. Additionally, they accelerated the development of experimental designs that would guarantee a performance edge over the Allied designs, designs that would replace the first German jet fighters, the [[Messerschmitt Me 262]] ''Schwalbe'' and [[Heinkel He 162]] ''Spatz''.

[[File:Wilhelm Busch's 'Hans Huckebein'.jpg|thumb|left|200px|A menacing "Hans Huckebein", the namesake raven for the Ta 183]]
The result was a series of advanced designs, some using [[swept wing]]s for improved [[transonic]] performance, others instead using the tailless design to lower drag to the same end. Since German aircraft engineers were aware that [[Tailless aircraft|tailless]] designs might encounter serious stability problems at transonic speeds, much as the prototype [[Messerschmitt Me 163#Later versions|Me 163B V18]] did on July 6, 1944, in hitting a record 1,130&nbsp;km/h (702&nbsp;mph) top speed and nearly destroying its entire rudder surface in the process,<ref>de Bie, Rob. [http://robdebie.home.xs4all.nl/me163/production.htm "Me 163B Komet - Me 163 Production - Me 163B: Werknummern list."] ''robdebie.home.'' Retrieved: 28 July 2013.</ref><ref>[http://www.walterwerke.co.uk/walter/me163c1a.htm "Me 163."] ''walterwerke.co.uk''. Retrieved: 28 August 2010.</ref> a variety of stabilization methods such as airbrakes on the wings were considered for such aircraft or simply adding conventional tail surfaces. [[Kurt Tank]]'s design team led by [[Hans Multhopp]] designed in 1945 a fighter known as "''Huckebein''" (from Wilhelm Busch's "''Hans Huckebein'', the unlucky raven", a cartoon raven that traditionally makes trouble for others), also known as Project V (Project VI in some references) or Design II at Focke-Wulf. The raven character itself was re-used for the modern Bundeswehr's ''[[Lufttransportgeschwader 62]]'' as the inspiration for their unit's insignia.

==Design==
[[File:Ta 183 Modell.jpg|thumb|Focke-Wulf Ta 183 Design&nbsp;II model]]
[[File:Ta183 Endversion Modell kl1.png|thumb|Final Ta 183 Design&nbsp;III model]]
[[File:Ta183B Modell kl2.png|thumb|Ta 183 B model]]
[[File:Fw SuperLorin Modell kl3.png|thumb|[[Focke-Wulf Super Lorin|Fw Super-Lorin]] model]]
Development of the Ta 183 started as early as 1942 as '''Project VI''', when the engineer [[Hans Multhopp]] assembled a team to design a new fighter, based on his understanding that previous Focke-Wulf design studies for jet fighters had no chance of reaching fruition because none had the potential for [[transonic]] speeds. This aircraft, bearing the RLM airframe number '''8-183''', was intended to use, as with [[Heinkel HeS 011#Intended applications|a growing number of other advanced German late-war jet aircraft proposals]], the advanced [[Heinkel HeS 011]] [[turbojet]]; although the first prototypes were to be powered by the [[Junkers Jumo 004]]B. Early studies also included an optional 1,000&nbsp;[[kilogram-force|kgf]] (10&nbsp;[[kilonewton|kN]]) thrust [[rocket engine]] for takeoff and combat boost, much as the special "003R" version of the [[BMW 003]] jet engine was meant to use, with fuel and oxidiser for up to 200 seconds of burn time stored in [[drop tank]]s under the wings.

The wings were swept back at 40° and were mounted in the mid-[[fuselage]] position. The wings appear to be mounted very far forward compared with most designs, a side-effect of attempting to keep the [[Center of pressure (fluid mechanics)|centre of pressure]] (CoP) of the wing as a whole as close to the middle of the fuselage as possible. Reflecting the dilemma of a shortage of [[strategic material]]s, the first option of using [[Aluminium|aluminum]] in the construction of the main [[Spar (aviation)|spar]] consisting of two tapered I-beams attached together on the top and bottom with shear webs of thin steel sheeting, led to a reappraisal. Multhopp chose to use wood instead of metal throughout the wing structure, with wood structure [[Rib (aircraft)|rib]]s attached to the front and back of the I-beams to give the wing its overall shape, and then covered with [[plywood]]. The box-like structure contained six [[Fuel tank#Aircraft|fuel cell]]s, giving the aircraft a total fuel load of 1,565&nbsp;L (413&nbsp;US gal).<ref>Myhra 1999, p. 7.</ref>

The original design used a [[T-tail]], with a notably long [[vertical stabilizer]] and a seemingly undersized [[Tailplane|horizontal stabilizer]]. The vertical stabilizer was swept back at 60°, and the horizontal stabilizer was swept back and slightly [[Dihedral (aircraft)|dihedral]]led. The horizontal stabilizer also featured two large trim tabs, the main pitching force actually being provided by what would have appeared to be "ailerons" on most other turbojet-powered fighter airframes of the period. The Ta 183 wing's outermost trailing-edge control surfaces on its wing panels, were well behind the [[center of gravity]], placing their trailing edges' tips virtually even, horizontally, with the intended HeS 011 jet engine's exhaust orifice, and thus could provide both pitch and roll control through functioning as [[elevon]] control surfaces, as those on the wing panels of Messerschmittt's [[Me 163]] tailplane-less ''Komet'' rocket fighter already did. Many problems beset the project, including the chance of a [[Dutch roll]]. Work therefore concentrated on the much less problematic [[Focke-Wulf Project VII]]. However, when the RLM eventually rejected that design, ''Huckebein'' was again brought to the fore.

The Ta 183 had a short fuselage with the air intake passing under the [[cockpit]] and proceeding to the rear where the single engine was located. The pilot sat in a [[Cabin pressurization|pressurized]] cockpit with a [[bubble canopy]] which provided excellent vision. The primary armament of the aircraft consisted of four 30&nbsp;mm (1.18&nbsp;in) [[MK 108 cannon]]s arranged around the air intake.

It was also possible to carry a bomb load of 500&nbsp;kg (1,100&nbsp;lb), consisting of one SD or more SC 500 half-tonne bombs, one ''Bombentorpedo'' BT 200 bomb, five SD-series fragmentation bombs, SC-series general-purpose bombs, or a Rb 20/30 reconnaissance camera. The weapons load would be carried in the equipment space in the bottom of the fuselage and thus partially protrude about halfway from the fuselage, possibly allowing for other armament packages such as the [[Ruhrstahl X-4]] wire-guided missile.

Multhopp's team also seriously explored a second version of the basic design, known as '''Design III''', a modified  '''Design II''' (it is unknown what Design I referred to). The first of these had only minor modifications, with slightly differently shaped wingtips and repositioning of the [[Landing gear|undercarriage]]. The second version had a reduced sweepback to 32°, allowing the wing and cockpit to be moved rearward. The tail was also redesigned, using a short horizontal boom to mount the control surfaces just above the line of the rear fuselage. This version looks considerably more "conventional" to the modern eye, although somewhat stubby due to the short overall length of the HeS 011.

The second of these two schemes was entered in the official competition ordered by the ''Oberkommando der Luftwaffe'' at the end of 1944. On 28 February 1945, the Luftwaffe High Command examined the various Emergency Fighter proposals and selected the [[Junkers EF 128]] to be developed and produced; the Focke-Wulf team gained second place. However, in the last few weeks of the war, it was decided that the ''Huckebein'' was really the best design and, at a meeting in [[Bad Eilsen]], Tank was told to arrange mockups and to plan for full production. It had a planned speed of about 1,000&nbsp;km/h (620&nbsp;mph) at 7,000&nbsp;m (22,970&nbsp;ft) and it was estimated that 300 aircraft per month would be delivered when production got into its stride, each aircraft being produced in 2,500 man hours.

A total of 16 [[prototype]]s were to be built, allowing the tail unit to be interchanged between the Design II and III variations. Of the ''Versuchs'' (experimental test series) aircraft, the Ta 183 V1-V3 were to be powered by the Jumo 004B turbojet with somewhat lengthened rear fuselages near the engine's exhaust nozzle to accommodate them, pending delivery of the HeS 011 jet engine. The Ta 183 V4-V14 were intended to be A-0 series pre-production aircraft and V15-V16 were to be static test aircraft. The first flight of the aircraft was projected for May 1945, but no finished Ta 183 ''Versuchs''-series prototypes had been completed by 8 April 1945, when British troops captured the Focke-Wulf facilities.

===Influence===
[[File:Pulqui II 04.jpg|thumb|Pulqui II on takeoff]]

After the end of the war, [[Kurt Tank]], in exile in Argentina, resurrected the Ta 183 project, resulting in the [[IAe Pulqui II]].<ref>Myrha 1999, pp. 7–10.</ref> This version was modified to place the wings at a shoulder-mounted position, in order to avoid a heavy fuselage spar pass-through structure going around the engine, however this resulted in [[Stall (flight)#Deep stall|deep stall]] problems at high angles of attack. This could be resolved, and a version correcting these problems was planned. However, the financial crash of 1953((clarify|date=February 2018)) and the fall of [[Juan Peron]] temporarily suspended work on the project. By 1955, the project had been abandoned due to the availability of surplus ex-[[Korean War]] [[North American F-86 Sabre|F-86 Sabres]] at a fraction of the cost.((citation needed|date=February 2018))

[[File:MiG-15 RB1.jpg|right|thumb|The MiG-15, which bears a resemblance to both the Ta 183 and Me 263.]]
Historians including David Myrha<ref>Myrha 1999, pp. 10, 11.</ref> have claimed the Soviet [[Mikoyan-Gurevich MiG-15]] was at least inspired by the Ta 183, because the Soviets captured plans from the Germans at the end of World War II. The MiG-15 does bear a resemblance in layout, sharing the high tailplane and nose-mounted intake, although the aircraft are different in structure, details, and proportions. The MiG-15's design shared features, and some appearance commonalities with the MiG design bureau's [[Mikoyan-Gurevich I-270|own 1945-46 attempt at a Soviet-built rocket interceptor]] similar to the [[Messerschmitt Me 263]] rocket fighter, and also common to many contemporary jet fighters — and were derived from aerodynamic and structural considerations (for example, the American [[Republic F-84F Thunderstreak|Republic F-84F]], the Swedish [[Saab 29 Tunnan|SAAB 29]], and the French [[Dassault Ouragan]] and [[Dassault Mystère|Mystère]]). A detailed design history of the MiG-15 was published by Russian aviation historian Yefim Gordon<ref>Gordon 2001,  pp. 3–6.</ref> refuting any connection between the Ta 183 and the MiG-15. According to the designers, the MiG-15 was an indigenous design, their choice of swept wings (as swept-back wings of any sort on a Soviet-designed aircraft were first flown on the [[Mikoyan-Gurevich MiG-8|MiG-8]] ''Utka'' canard light aircraft of 1945) being due to their desire to move ahead of most Western designs which were not intended for the 960&nbsp;km/h+ (600&nbsp;mph+) speed range.

Like the MiG-9 and MiG-15, the Saab 29 is subject to claims of having been indirectly influenced by the Ta 183. SAAB engineers received German research studies in swept wings in the immediate post-war period via contacts in [[Switzerland]], and incorporated it into the Tunnan design, which was still limited to paper studies at the time.<ref>Erichs et al. 1988, p. 37.</ref>

==Specifications (Ta 183, as originally designed)==
[[File:Focke-Wulf Ta 183 3-view line drawing.svg|right|300px]]
((Aircraft specs
|ref=Jet Planes of the Third Reich<ref name=Creek>((cite book |last1=Creek |first1=Eddie J. |last2=Smith |first2=J. Richard |date=1982 |title=Jet Planes of the Third Reich |location=Boylston, MA USA |publisher=Monogram Aviation Publications |pages=384–387 |isbn=0-914144-27-8 ))</ref>
|prime units?=met
<!--
        General characteristics
-->
|crew=1
|length m=9.4
|length note=
|span m=10
|span note=
|height m=3.86
|height note=
|wing area sqm=22.5
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil=
|empty weight kg=2830
|empty weight note=
|gross weight kg=4300
|gross weight note=
|max takeoff weight kg=
|max takeoff weight note=
|fuel capacity=
|more general=
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=[[Heinkel HeS 011]]
|eng1 type=[[turbojet]]
|eng1 kn=13
|eng1 note=
<!--
        Performance
-->
|max speed kmh=955
|max speed note=
|cruise speed kmh=
|cruise speed note=
|stall speed kmh=
|stall speed note=
|never exceed speed kmh=
|never exceed speed note=
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|range km=
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|combat range km=
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|ceiling m=14000
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ms=20.4
|climb rate note=
|time to altitude=
|wing loading kg/m2=196
|wing loading note=
|fuel consumption kg/km=
|thrust/weight=0.37
|more performance=<!--</br>
*'''Take-off run:''' ((cvt||m|0))
*'''Take-off run to ((cvt|15|m|0)):''' ((cvt||m|0))
*'''Landing run:''' ((cvt||m|0))
*'''Landing run from ((cvt|15|m|0)):''' ((cvt||m|0))-->
<!--
        Armament
-->
|guns=4 × [[30 mm caliber|30 mm]] (1.18 in) [[MK 108 cannon]]
|bombs= 500 kg (1,102 lb) of bombs
|rockets= 
|missiles= 4 × [[Ruhrstahl X-4]] Wire Guided AAMs
|hardpoints=4

|avionics=
))

==See also==
((aircontent|
|related=
* [[Focke-Wulf Flitzer]]
* [[Focke-Wulf Super Lorin]]
* [[Focke-Wulf Volksjäger]]
* [[Focke-Wulf Ta 283]]
* [[FMA IAe 33 Pulqui II]]
|similar aircraft=
* [[Lavochkin La-15]]
* [[Mikoyan-Gurevich MiG-15]]
* [[Messerschmitt Me P.1101]]
* [[Saab 29 Tunnan]]
))

==References==
'''Notes'''
((Reflist))

'''Bibliography'''
((Refbegin))
* Ciampaglia, Giuseppe. ''Il Focke Wulf Ta-183. Il capostipite dei caccia a getto di seconda generazione''. Rivista Italiana Difesa, gennaio, 2013.
* Erichs, Rolph et al. ''The Saab-Scania Story''. Stockholm: Streiffert & Co., 1988. ((ISBN|91-7886-014-8)).
* Gordon, Yefim. ''Mikoyan-Gurevich MiG-15: The Soviet Union's Long-Lived Korean War Fighter''. Earl Shilton, Leicester, UK: Midland Publishing Ltd., 2001. ((ISBN|1-85780-105-9)).
* Myhra, David. ''Focke-Wulf Ta 183'' (X Planes of the Third Reich). Atglen, Pennsylvania: Schiffer Publishing, 1999. ((ISBN|0-7643-0907-2)).
((Refend))

==External links==
((Commons category|Focke-Wulf Ta 183))

((Focke-Wulf aircraft))
((Kurt Tank aircraft))
((RLM aircraft designations))
((Authority control))

[[Category:Focke-Wulf aircraft|Ta 183]]
[[Category:Abandoned military aircraft projects of Germany]]
[[Category:World War II jet aircraft of Germany]]
[[Category:Single-engined jet aircraft]]
[[Category:High-wing aircraft]]
[[Category:Nose-mounted intake jet fighter]]

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