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Arado Ar 240

The Arado Ar 240 was a German twin-engine, multi-role heavy fighter aircraft, developed for the Luftwaffe during World War II by Arado Flugzeugwerke. Its first flight was on 10 May 1940,[1] but problems with the design hampered development, and it remained only marginally stable throughout the prototype phase. The project was eventually cancelled, with the existing airframes used for a variety of test purposes.

Ar 240
Model of an Ar 240
Role Zerstörer (Destroyer) prototype
National origin Germany
Manufacturer Arado Flugzeugwerke
First flight 10 May 1940
Primary user Luftwaffe
Number built 15

Design and development edit

The Ar 240 came about as the response to a 1938 request for a much more capable second-generation heavy fighter to replace the Messerschmitt Bf 110, which was becoming outdated. Both Arado and Messerschmitt responded. Messerschmitt's response, the Me 210, was a totally new design, but thanks to Messerschmitt's experience with the Zerstörer ("Destroyer") concept, it would be able to enter service quickly. Arado's design was considerably more ambitious for the smaller firm, a dream project of Arado's chief designer, Walter Blume, since the mid-1930s. While it would take some time before deliveries of the Arado design could begin, the Reichsluftfahrtministerium (RLM/German Aviation Ministry) was nevertheless interested enough to order prototypes of both designs.[2]

Prior to this point, Arado had invested heavily in several lines of basic research. One was the development of the "Arado travelling flap" which offered excellent low-speed lift performance. Another was ongoing work in the design and construction of pressurized cockpits, which dramatically lowered pilot fatigue for any flight above about 4,500 m (14,760 ft). Finally, they had also invested in a technically advanced remote-control defensive gun system, which they had been experimenting with for several years. The system used a gunsight located in the rear cockpit, operated by the navigator/gunner, which had optics on both the top and bottom of the aircraft, allowing aim in any direction. The gunsight was hydraulically connected to well-streamlined pancake-shaped, remotely-operated turrets on the top and bottom of the aircraft. For the Ar 240 design, the Arado engineers combined all this research into a single airframe.

For outright performance, they used as small a wing as reasonable, thereby lowering parasite drag (at the expense of greater lift-induced drag). Normally this would make the plane have "impossibly high" landing speeds, but this was offset by the use of a huge travelling flap and leading edge slats for high low-speed lift. When the flaps were extended, the upper portion of the ailerons would remain in place while the lower portion extended rearward, essentially increasing the wing area.

 
A Jumo 222-powered Junkers Ju 288 prototype with ducted spinners, of a similar type to that intended for the Ar 240.

The Daimler-Benz DB 601 inline engines were conventionally installed and equipped with three-blade, fully adjustable propellers. The radiators were somewhat unusual however, quite similar to those fitted to the Junkers Ju 88 which pioneered them - but much more closely resembling the intended installation of the radiators intended for the Junkers Ju 288, when powered by its intended multibank Junkers Jumo 222 liquid-cooled 24-cylinder engines - for both types, consisting of an annular block located in front of each engine, but with the Ar 240 partially covering each of them with an oversized, ducted flow-through propeller spinner forward of each radiator unit, with air entering through a large hole in the front of the spinner and exiting out of the cowl flaps, as the Jumo 222-powered Ju 288 design was intended to have.[3] As with the Jumo inline-powered versions of the Ju 88, this made the plane look as if it were mounting a radial engine, and the Ar 240, like later Jumo inline-powered fighter aircraft from the Focke-Wulf firm (the Fw 190D, Ta 152 and twin-engined Ta 154) also benefitted from the simpler setup of an annular radiator just forward of the engine.

The fuel cells in the wings were provided with a newly developed self-sealing system that used thinner tank liners, allowing for more fuel storage. The liners could not be easily removed as they stuck to the outer surface of the tank, so in order to service them, the wing panelling had to be removable. This led to a complex system for providing skinning stiff enough to be handled in the field, complicating construction and driving up weight.

As with all German multi-use aircraft designs of the era, the aircraft was required to be a credible dive bomber. The thick wing panelling was not suitable for piercing for conventional dive brakes, so a "petal"-type brake was installed at the extreme rear of the fuselage — appearing much like what had been trialled with the Dornier Do 217 — which, unlike the Do 217's vertically-opening "petals", opened to the sides instead when activated. When closed the brake looked like a stinger, extending beyond the horizontal stabilizer and twin fins.

Finally, the cockpit was fully pressurized. This would not have been easy if the armament had to be hand-operated by the gunner, as it would have required the guns to penetrate the rear of the cockpit canopy. However, the remote control system allowed them to be located in turrets in the unpressurized rear of the fuselage.

All of this added weight, and combined with the small wing, led to a very high wing loading of 330 kg/m2 (221 lb/ft2), compared to an average of about a 100 for a single-seat fighter.

Operational history edit

Testing and evaluation edit

Technical specifications were first published in October 1938, followed by detailed plans later that year. In May 1939, the RLM ordered a batch of six prototypes. The first Ar 240 V1 prototype, DD+QL, took to the air on 25 June 1940, and immediately proved to have poor handling in all axes, also tending to overheat during taxiing.

The handling was thought to be the result of the ailerons being too small, given the thick wing, so the second prototype was modified to have larger ones, as well as additional vertical fin area on the dive brakes to reduce yaw. In addition, small radiators were added to the landing gear legs to improve cooling at low speeds, when the gear would normally be opened. Ar 240 V2, KK+CD, first flew on 6 April 1941, and spent most of its life at the factory in an experimental role.

Ar 240 V3 followed, the first to be equipped with the FA 9 rear-firing armament system, developed jointly by Arado and DVL, armed with a 7.92 mm (.312 in) MG 81Z machine gun. Ar 240 V4 was the first to include an operational dive brake, and flew on 19 June 1941. Ar 240 V5 and the V6 followed in December and January, including the upgraded FA 13 system, using two 13 mm (.51 in) MG 131 machine guns in place of the MG 81Z for a considerable boost in firepower.[2] Ar 240 V7 and V8 acted as prototypes for the planned Ar 240B, which was to use two Daimler Benz DB 605As, while Ar 240 V9, V10, and V11, and V12 served as prototypes of the Ar 240C.[4]

The Ar 240's excellent performance quickly led to the V3, V5 and V6 being stripped of their armament, including the defensive guns, and used as reconnaissance aircraft over England, where no other two-seater could venture by 1942. The five AGO Flugzeugwerke built Ar 240A-0 saw operational service in 1943. JG 5 'Eismeer', based in Finland, received two, 1. and 3.(F)/100 on the Eastern Front (World War II) received one each and 1.(F)/123 in Italy received one.[1]

Variants edit

 
Arado Ar 440
Ar 240A-0
Four preproduction aircraft.
Ar 240B
Proposed version
Ar 240C-1
Heavy fighter version.
Ar 240C-2
Night fighter version.
Ar 240C-3
Light bomber version.
Ar 240C-4
High-altitude reconnaissance version. The project was abandoned in favour of the Ar 440.
Ar 440
Ar 240 V10 was earmarked as the Ar 440 prototype; second prototype not built.[5] Improved variant with the fuselage stretched by 0.9m (35.5 in) and powered by the 1,900 hp (1,417 kW) DB 603G, the production aircraft would have had two 2,000 hp (1,491 kW) DB 627A/B engines. Planned armament was two 13mm MG 131s, three 20mm MG 151s and two 30mm MK 108 cannons, plus 1,000kg bomb load. First flown in early Summer 1942, it proved far superior to the Ar 240. Production was eventually rejected in favour of the Dornier Do 335.[1]

Specifications (Ar 240A-01) edit

Data from [6]

General characteristics

  • Crew: two
  • Length: 12.81 m (42 ft 0 in)
  • Wingspan: 13.34 m (43 ft 9 in)
  • Height: 3.95 m (13 ft 0 in)
  • Wing area: 31.3 m2 (337 sq ft)
  • Aspect ratio: 5.68
  • Empty weight: 6,200 kg (13,669 lb)
  • Gross weight: 9,450 kg (20,834 lb)
  • Max takeoff weight: 10,297 kg (22,701 lb)
  • Powerplant: 2 × Daimler-Benz DB 601E inverted V-12 liquid-cooled piston engine, 876 kW (1,175 hp) each
  • Propellers: 3-bladed constant speed metal propellers

Performance

  • Maximum speed: 618 km/h (384 mph, 334 kn)
  • Cruise speed: 555 km/h (345 mph, 300 kn)
  • Range: 2,000 km (1,200 mi, 1,100 nmi)
  • Service ceiling: 10,500 m (34,400 ft)
  • Rate of climb: 9.083 m/s (1,788.0 ft/min)
  • Time to altitude: Climb to 6,000 m (19,700ft): 11 min
  • Wing loading: 302 kg/m2 (62 lb/sq ft)
  • Power/mass: 0.19 kW/kg (0.11hp/lb)

Armament

See also edit

Aircraft of comparable role, configuration, and era

Related lists

References edit

  1. ^ a b c Munson 1978, p. 26.
  2. ^ a b Gunston 1989, p. 157.
  3. ^ Ju 288 nacelles for Jumo 222 engines, showing the flow-through ducted spinners
  4. ^ "Luftwaffe Lovers: Multirole aircraft - Arado Ar240". 4 June 2016.
  5. ^ Griehl, Manfred, X-Planes: German Luftwaffe Protoytpes 1930-1945, Barnsley, South Yorkshire, UK: Frontline Books, 2012, ISBN 9781783034192, unpaginated.
  6. ^ Green, William (2010). Aircraft of the Third Reich. Vol. 1 (1st ed.). London: Aerospace Publishing Limited. pp. 85–90. ISBN 978-1-900732-06-2.

Bibliography edit

  • Green, William. Warplanes of the Third Reich. London: Macdonald and Jane's Publishers Ltd., Fourth impression 1979, First edition 1970. ISBN 0-356-02382-6.
  • Gunston, Bill. Jane's Fighting Aircraft of World War II. New York: Jane's Publishing/Random House, 1989, First edition 1945. ISBN 1-85170-493-0.
  • Lang, Gerhard. Arado Ar 240 (Luftwaffe Profile Series No.8). Atglen, PA: Schiffer Publishing, 1997. ISBN 0-88740-923-7.
  • Munson, Kenneth (1978). German Aircraft Of World War 2 in colour. Poole, Dorsett, UK: Blandford Press. ISBN 0-7137-0860-3.
  • Smith, J.R. and Anthony L. Kay. German Aircraft of the Second World War. London: Putnam & Company Ltd., 1972. ISBN 0-370-00024-2.

External links edit

arado, german, twin, engine, multi, role, heavy, fighter, aircraft, developed, luftwaffe, during, world, arado, flugzeugwerke, first, flight, 1940, problems, with, design, hampered, development, remained, only, marginally, stable, throughout, prototype, phase,. The Arado Ar 240 was a German twin engine multi role heavy fighter aircraft developed for the Luftwaffe during World War II by Arado Flugzeugwerke Its first flight was on 10 May 1940 1 but problems with the design hampered development and it remained only marginally stable throughout the prototype phase The project was eventually cancelled with the existing airframes used for a variety of test purposes Ar 240 Model of an Ar 240 Role Zerstorer Destroyer prototype National origin Germany Manufacturer Arado Flugzeugwerke First flight 10 May 1940 Primary user Luftwaffe Number built 15 Contents 1 Design and development 2 Operational history 2 1 Testing and evaluation 3 Variants 4 Specifications Ar 240A 01 5 See also 6 References 7 Bibliography 8 External linksDesign and development editThe Ar 240 came about as the response to a 1938 request for a much more capable second generation heavy fighter to replace the Messerschmitt Bf 110 which was becoming outdated Both Arado and Messerschmitt responded Messerschmitt s response the Me 210 was a totally new design but thanks to Messerschmitt s experience with the Zerstorer Destroyer concept it would be able to enter service quickly Arado s design was considerably more ambitious for the smaller firm a dream project of Arado s chief designer Walter Blume since the mid 1930s While it would take some time before deliveries of the Arado design could begin the Reichsluftfahrtministerium RLM German Aviation Ministry was nevertheless interested enough to order prototypes of both designs 2 Prior to this point Arado had invested heavily in several lines of basic research One was the development of the Arado travelling flap which offered excellent low speed lift performance Another was ongoing work in the design and construction of pressurized cockpits which dramatically lowered pilot fatigue for any flight above about 4 500 m 14 760 ft Finally they had also invested in a technically advanced remote control defensive gun system which they had been experimenting with for several years The system used a gunsight located in the rear cockpit operated by the navigator gunner which had optics on both the top and bottom of the aircraft allowing aim in any direction The gunsight was hydraulically connected to well streamlined pancake shaped remotely operated turrets on the top and bottom of the aircraft For the Ar 240 design the Arado engineers combined all this research into a single airframe For outright performance they used as small a wing as reasonable thereby lowering parasite drag at the expense of greater lift induced drag Normally this would make the plane have impossibly high landing speeds but this was offset by the use of a huge travelling flap and leading edge slats for high low speed lift When the flaps were extended the upper portion of the ailerons would remain in place while the lower portion extended rearward essentially increasing the wing area nbsp A Jumo 222 powered Junkers Ju 288 prototype with ducted spinners of a similar type to that intended for the Ar 240 The Daimler Benz DB 601 inline engines were conventionally installed and equipped with three blade fully adjustable propellers The radiators were somewhat unusual however quite similar to those fitted to the Junkers Ju 88 which pioneered them but much more closely resembling the intended installation of the radiators intended for the Junkers Ju 288 when powered by its intended multibank Junkers Jumo 222 liquid cooled 24 cylinder engines for both types consisting of an annular block located in front of each engine but with the Ar 240 partially covering each of them with an oversized ducted flow through propeller spinner forward of each radiator unit with air entering through a large hole in the front of the spinner and exiting out of the cowl flaps as the Jumo 222 powered Ju 288 design was intended to have 3 As with the Jumo inline powered versions of the Ju 88 this made the plane look as if it were mounting a radial engine and the Ar 240 like later Jumo inline powered fighter aircraft from the Focke Wulf firm the Fw 190D Ta 152 and twin engined Ta 154 also benefitted from the simpler setup of an annular radiator just forward of the engine The fuel cells in the wings were provided with a newly developed self sealing system that used thinner tank liners allowing for more fuel storage The liners could not be easily removed as they stuck to the outer surface of the tank so in order to service them the wing panelling had to be removable This led to a complex system for providing skinning stiff enough to be handled in the field complicating construction and driving up weight As with all German multi use aircraft designs of the era the aircraft was required to be a credible dive bomber The thick wing panelling was not suitable for piercing for conventional dive brakes so a petal type brake was installed at the extreme rear of the fuselage appearing much like what had been trialled with the Dornier Do 217 which unlike the Do 217 s vertically opening petals opened to the sides instead when activated When closed the brake looked like a stinger extending beyond the horizontal stabilizer and twin fins Finally the cockpit was fully pressurized This would not have been easy if the armament had to be hand operated by the gunner as it would have required the guns to penetrate the rear of the cockpit canopy However the remote control system allowed them to be located in turrets in the unpressurized rear of the fuselage All of this added weight and combined with the small wing led to a very high wing loading of 330 kg m2 221 lb ft2 compared to an average of about a 100 for a single seat fighter Operational history editTesting and evaluation edit Technical specifications were first published in October 1938 followed by detailed plans later that year In May 1939 the RLM ordered a batch of six prototypes The first Ar 240 V1 prototype DD QL took to the air on 25 June 1940 and immediately proved to have poor handling in all axes also tending to overheat during taxiing The handling was thought to be the result of the ailerons being too small given the thick wing so the second prototype was modified to have larger ones as well as additional vertical fin area on the dive brakes to reduce yaw In addition small radiators were added to the landing gear legs to improve cooling at low speeds when the gear would normally be opened Ar 240 V2 KK CD first flew on 6 April 1941 and spent most of its life at the factory in an experimental role Ar 240 V3 followed the first to be equipped with the FA 9 rear firing armament system developed jointly by Arado and DVL armed with a 7 92 mm 312 in MG 81Z machine gun Ar 240 V4 was the first to include an operational dive brake and flew on 19 June 1941 Ar 240 V5 and the V6 followed in December and January including the upgraded FA 13 system using two 13 mm 51 in MG 131 machine guns in place of the MG 81Z for a considerable boost in firepower 2 Ar 240 V7 and V8 acted as prototypes for the planned Ar 240B which was to use two Daimler Benz DB 605As while Ar 240 V9 V10 and V11 and V12 served as prototypes of the Ar 240C 4 The Ar 240 s excellent performance quickly led to the V3 V5 and V6 being stripped of their armament including the defensive guns and used as reconnaissance aircraft over England where no other two seater could venture by 1942 The five AGO Flugzeugwerke built Ar 240A 0 saw operational service in 1943 JG 5 Eismeer based in Finland received two 1 and 3 F 100 on the Eastern Front World War II received one each and 1 F 123 in Italy received one 1 Variants edit nbsp Arado Ar 440 Ar 240A 0 Four preproduction aircraft Ar 240B Proposed version Ar 240C 1 Heavy fighter version Ar 240C 2 Night fighter version Ar 240C 3 Light bomber version Ar 240C 4 High altitude reconnaissance version The project was abandoned in favour of the Ar 440 Ar 440 Ar 240 V10 was earmarked as the Ar 440 prototype second prototype not built 5 Improved variant with the fuselage stretched by 0 9m 35 5 in and powered by the 1 900 hp 1 417 kW DB 603G the production aircraft would have had two 2 000 hp 1 491 kW DB 627A B engines Planned armament was two 13mm MG 131s three 20mm MG 151s and two 30mm MK 108 cannons plus 1 000kg bomb load First flown in early Summer 1942 it proved far superior to the Ar 240 Production was eventually rejected in favour of the Dornier Do 335 1 Specifications Ar 240A 01 editData from 6 General characteristicsCrew two Length 12 81 m 42 ft 0 in Wingspan 13 34 m 43 ft 9 in Height 3 95 m 13 ft 0 in Wing area 31 3 m2 337 sq ft Aspect ratio 5 68 Empty weight 6 200 kg 13 669 lb Gross weight 9 450 kg 20 834 lb Max takeoff weight 10 297 kg 22 701 lb Powerplant 2 Daimler Benz DB 601E inverted V 12 liquid cooled piston engine 876 kW 1 175 hp each Propellers 3 bladed constant speed metal propellers Performance Maximum speed 618 km h 384 mph 334 kn Cruise speed 555 km h 345 mph 300 kn Range 2 000 km 1 200 mi 1 100 nmi Service ceiling 10 500 m 34 400 ft Rate of climb 9 083 m s 1 788 0 ft min Time to altitude Climb to 6 000 m 19 700ft 11 min Wing loading 302 kg m2 62 lb sq ft Power mass 0 19 kW kg 0 11hp lb Armament Guns 2 fixed 7 92 mm 312 in MG 17 machine guns Two remote control turrets with 2 7 92 mm 312 in MG 81 machine guns Bombs 1 800 kg 4 000 lb bombsSee also editAircraft of comparable role configuration and era Messerschmitt Me 210 Messerschmitt Me 410 Hornisse Related lists List of aircraft of World War II List of German aircraft projects 1939 45 List of World War II military aircraft of GermanyReferences edit a b c Munson 1978 p 26 a b Gunston 1989 p 157 Ju 288 nacelles for Jumo 222 engines showing the flow through ducted spinners Luftwaffe Lovers Multirole aircraft Arado Ar240 4 June 2016 Griehl Manfred X Planes German Luftwaffe Protoytpes 1930 1945 Barnsley South Yorkshire UK Frontline Books 2012 ISBN 9781783034192 unpaginated Green William 2010 Aircraft of the Third Reich Vol 1 1st ed London Aerospace Publishing Limited pp 85 90 ISBN 978 1 900732 06 2 Bibliography editGreen William Warplanes of the Third Reich London Macdonald and Jane s Publishers Ltd Fourth impression 1979 First edition 1970 ISBN 0 356 02382 6 Gunston Bill Jane s Fighting Aircraft of World War II New York Jane s Publishing Random House 1989 First edition 1945 ISBN 1 85170 493 0 Lang Gerhard Arado Ar 240 Luftwaffe Profile Series No 8 Atglen PA Schiffer Publishing 1997 ISBN 0 88740 923 7 Munson Kenneth 1978 German Aircraft Of World War 2 in colour Poole Dorsett UK Blandford Press ISBN 0 7137 0860 3 Smith J R and Anthony L Kay German Aircraft of the Second World War London Putnam amp Company Ltd 1972 ISBN 0 370 00024 2 External links edit nbsp Wikimedia Commons has media related to Arado Ar 240 Retrieved from https en wikipedia org w index php title Arado Ar 240 amp oldid 1210985765, wikipedia, wiki, book, books, library,

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