World War II Bomber Aircraft

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 German World War II Bomber Aircraft


Dornier Do-215
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The Dornier Do 215 was a light bomber, reconnaissance aircraft and later a night fighter aircraft produced by Dornier Werke GmbH originally produced for export, but in the event all except two served in the Luftwaffe. It was nicknamed "The Flying Pencil" because of its slim fuselage. The successor of the Do 215 was the Dornier Do 217.

The Dornier Do 17 fast bomber elicited renewed interest from foreign air forces (after the initial Do 17K series production). In July 1937, Dornier therefore prepared a pre-series Do 17 Z-0 as a demonstrator for export customers. It was given the civil registration D-AAIV. While this aircraft was essentially identical to the production Do 17Z, the Reichsluftfahrtministerium assigned the designation Do 215 to the export version. The V1 prototype retained the 9-cylinder Bramo 323 Fafnir radial of the Do 17Z.

The second prototype (Do 215 V2) was equipped with Gnome-Rhône 14-NO radial engines. It safely completed testing, but did not attract export orders because it did not offer a notable performance increase over the Do 17Z. Dornier therefore equipped the V3 prototype with the 1,175 PS (1,159 hp) Daimler-Benz DB 601Ba inline engines (note: it is not the first time DB engines where used in a Do 17 series). The V3, which first flew in the spring of 1939, showed a noticeable improvement in flight performance compared to the earlier prototypes.

Series production of the Do 215 A-1 began in 1939. The order, intended for the Swedish Air Force, was stopped in August 1939 due to the political situation. The 18 extant aircraft were embargoed and pressed into Luftwaffe service upon the outbreak of World War II.

Some modifications were made and the resulting aircraft were redesignated Do 215B. This was the standard production version. Between 92 and 105 (depending on sources) were produced between 1939 and 1941.

The Luftwaffe initially operated the Do 215 as a bomber and reconnaissance aircraft. Aircraft equipped with the Rb 20/30 and Rb 50/30 cameras were used for long-range reconnaissance missions, primarily at the Ob.d.L (Oberkommando der Luftwaffe). Later aircraft operated as night fighters. The last of the Do 215s were retired in late 1944.

General characteristics

  • Crew: 4 (pilot, bomb aimer/gunner, two gunners)
  • Length: 15.79 m (51 ft 9 in)
  • Wingspan: 18 m (59 ft 0 in)
  • Height: 4.56 m (14 ft 11½ in)
  • Wing area: 55 m² (592 ft²)
  • Empty weight: 5,780 kg (12,727 lb)
  • Loaded weight: 8,800 kg (19,404 lb)
  • Powerplant: 2× Daimler-Benz DB 601 Ba [Daimler-Benz_DB-605B_V12]V-12-cylinder inline engines, 1,175 PS (1,159 hp, 864 kW) each

Performance

  • Maximum speed: 470 km/h (254 knots, 292 mph) at 4000 m (13,124 ft)
  • Range: 2,450km (1,323 nm, 1,522 mi) normal
  • Service ceiling 9,000 m (29,500 ft)
  • Wing loading: 105.1 kg/m² (32.78 lb/ft²)
  • Power/mass: 184 W/kg (0.113 hp/lb)

Armament

  • Four 7.92 mm MG 15 [Rheinmetall-Borsig_MG-15_7.92mm_MG]machine guns, later upgraded to 6
  • 1000 kg (2,200 lb) bombs

 


Dornier Do-217
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The Dornier Do 217 was a bomber used by Germany during World War II. It was designed from scratch as a replacement for the earlier Dornier Do 17.

At the beginning of 1938, Dornier issued manufacturing specification No. 1323, recognising the need for a twin engined bomber or long range reconnaissance aircraft powered by Daimler-Benz DB 601B engines. Dornier recognized shortcomings of its fast Dornier Do 17 well before the war. With Junkers' new prototype, the Junkers Ju 88 being superior to the Do 17 in every way, Dornier designed a new bomber to meet a requirement from the RLM for a larger and more versatile bomber than the Do 17, capable of both level and dive bombing. One of the most versatile and useful bomber designs the Germans put into production after the war started, the Dornier Do 217 remedied the shortcomings of the Do 17 while greatly advancing the design in all areas.

Superficially a scaled up Dornier Do 215, and initially powered by the same engines, the Do 217 was actually considerably larger and totally different in detailed design. The first prototype (the Do 217 V1) flew on 4 October 1938, but crashed seven days later during a single engine flying test.[1] It was found to be underpowered and was unmanoeuvrable when compared with contemporary bombers. Instability was a problem at first, but modifications such as fixed slats along the leading edges of the vertical fins helped to improve flight stability.

Much of Dornier's efforts in 1938 to 1940 were devoted to finding more powerful engines and improving the flying qualities. When the BMW 801 radial engine became available, it solved the problems of the aircraft being underpowered and allowed the fuselage to be deepened, thus accommodating larger and heavier bomb loads. This enabled the Do 217 to fulfil its potential and carry a heavier bomb load than any other Luftwaffe bomber of the time.

There was a desire for the Do 217 to be capable of performing dive bomber duty, so it was therefore fitted with a tail mounted air brake. This could not be made to function adequately in the early models however, and was omitted until the Do 217E-2 entered service. When this mark reached service, use of the dive brake was found to sometimes overstrain the rear fuselage, so the dive brakes were often removed.

In almost every way, the Do 217 was a success. It could carry a much heavier bombload than either the Heinkel He 111 or the Junkers Ju 88. It was also very fast, surpassing both aircraft in maximum speed. It was Germany's largest bomber for nearly two years until the Heinkel He 177 was finally safe enough to use. Do 217s sank the Italian battleship Roma with Fritz X missiles as she steamed to the Allies after Italy's capitulation. Do 217s were phased out of combat use in mid 1944.

Like the Do 17 and the Ju 88, the aircraft was used in a variety of roles, including that of the night-fighter - a sign that Germany desperately needed fighters far more than it needed bombers. Production was stopped in April 1944 in favor of single-engined fighters. Operational use of the Do 217 as a night-fighter was restricted in 1943 to NJG 4. The only capability in which the Do 217 was used up to the end of the war was as a night reconnaissance plane. Like the Do 17, this important type of service in the Luftwaffe is frequently overlooked.

The Do 217 was built in series from November 1940 to May 1944. In 1943, 395 aircraft could not be delivered to the Luftwaffe due to shortages of the DB 603 engines used in the M-1 and N-1 versions. These aircraft were stored, and while some were refitted in 1944 when the engines became available, the remainder (around 125) were scrapped. The Do 217 was only built by the three Dornier companies: Dornier Friedrichshafen (DWF): 316 aircraft, Dornier München (DWM): 985 aircraft and Norddeutsche Dornier-Werke (NDW): 602 aircraft. Production stopped in Friedrichshafen in December 1942, and in Wismar (NDW) in October 1943.

General characteristics

  • Crew: 3
  • Length: 18.20 m (59 ft 8½ in)
  • Wingspan: 19.00 m (62 ft 4 in)
  • Height: 5.00 m (16 ft 5 in)
  • Wing area: 57.00 m² (613.54 ft²)
  • Empty weight: 9,350 kg (20,615 lb)
  • Max takeoff weight: 13,180 kg (29,059 lb)
  • Powerplant: 2× BMW 801A [BMW_801_14cyl_Radial]14-cylinder radial engine, 1,560 PS (1,539 hp, 1,147 kW) each

Performance

  • Maximum speed: 487 km/h at 5,500 m (303 mph at 18,045 ft)
  • Range: 2,050 km (1,274 miles)
  • Service ceiling 8,400 m (27,560 ft)

Armament

  • 4 x 7.92 mm MG 17 [Rheinmetall-Borsig_MG-17_7.92mm_MG]machine guns in nose with 1,000 rpg
  • 4 x 20 mm MG FF [Ikaria_Werke_MG_FF-M_20mm_Cannon]cannons in nose with 250 rpg
  • 2 x 13 mm MG 131 [MG_131_13mm_MG]machine guns in dorsal and ventral positions with about 500 rpg apiece

 


Heinkel He-111
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The Heinkel He 111 was a German medium bomber designed by Siegfried and Walter Günter in the early 1930s in violation of the Treaty of Versailles. The Heinkel became the most numerous and primary Luftwaffe bomber during the early stages of World War II. It is perhaps the most famous symbol of the German bomber force (Kampfwaffe) due its distinctive "Greenhouse" nose.

The He 111 took on the mantle of "workhorse", and was used in a variety of roles on every front in the European Theatre throughout the war. It was used as a strategic bomber during the Battle of Britain, a torpedo bomber during the Battle of the Atlantic, a medium bomber and a transport aircraft on the Western Front, Eastern Front and Mediterranean and North African Fronts. It became obsolete, but the failure to design and produce a successor meant the He 111 continued to be produced until 1944, when piston-engined bomber production was largely halted, in favour of fighter aircraft.

The design of the Heinkel endured after the war in the CASA 2.111. Its airframe was produced in Spain under license by Construcciones Aeronáuticas SA. The design differed significantly in powerplant only. The Heinkel's descendant continued in service until 1973, when it was retired.

In the early 1930s, Ernst Heinkel decided to build the world's fastest passenger plane, a lofty goal met by more than a little skepticism by the German aircraft industry and its newly evolving political leadership. Heinkel entrusted the development to Siegfried and Walter Günter, fairly new to the company and untested.

The aircraft was superior to the already fast Lockheed 9 Orion that their design was competing against. The first example of their soon-to-be-famous Heinkel He 70 Blitz (“Lightning”) rolled off the line in 1932 and immediately started breaking records. In its normal four-passenger version, its speed almost reach 200 mph (320 km/h), even though it was powered by only a single 600 hp (447 kW) BMW V1 engine. The elliptical wing, which the Günther brothers had already used in the Bäumer Sausewind sports plane before they joined Heinkel, became a feature in many subsequent designs the brothers developed. The design immediately garnered the interest of the Luftwaffe, which was looking for medium bombers for military service.

The future Heinkel He 111 was a more powerful twin-engine version of the Blitz, producing an aircraft that had many of the Blitz's features, including its elliptical inverted gull wing, small rounded control surfaces, and BMW engines. With location of the engines the only notable change in appearance, the new He 111 design was often called the Doppel-Blitz (“Double Lightning”).

At 14,000 kg take-off weight (carrying 2,000 kg of bombs internally), the He 111H achieved a top speed of 405 km/h at 6 km, improving to 435 km/h without the bomb load and at 50% fuel load. Still, this was considerably slower than the newer Junkers Ju 88 which entered service in 1940, so the He 111 was gradually withdrawn from the bomber role. The He 111 became a jack-of-all-trades as the war progressed, carrying out missions not even imagined when the war started.

Nevertheless, the He 111 had to be kept in production until 1944 because the RLM failed to provide a successor: the He 177 Greif heavy bomber was plagued by engine problems, and the Bomber B program was eventually abandoned. The vast majority of the 7,300 He 111s produced would be the H models, largely identical to the first H introduced in 1939.

General characteristics

  • Crew: 5 (pilot, navigator/bombardier, nose gunner, ventral gunner, dorsal gunner)
  • Length: 16.4 m (54 ft 6 in)
  • Wingspan: 22.5 m (74 ft 3 in)
  • Height: 3.9 m (13 ft 9 in)
  • Wing area: 86.5 m² (942 ft²)
  • Empty weight: 7,720 kg (17,000 lb)
  • Loaded weight: 12,030 kg (26,500 lb)
  • Max takeoff weight: 14,075 kg (31,000 lb)
  • Powerplant: 2× Jumo 211F-1 [Jumo_211F-1_inverted_V-12]liquid-cooled inverted V-12, 986 kW (1,300 hp) each

Performance

  • Maximum speed: 400 km/h (250 mph)
  • Range: 2,800 km with max fuel (1,750 mi)
  • Service ceiling 8,390 m (27,500 ft)
  • Rate of climb: 20 minutes to 5,185 m (17,000 ft)
  • Wing loading: 137 kg/m² (28.1 lb/ft²)
  • Power/mass: .082 kW/kg (.049 hp/lb)

Armament

  • Guns:
    • up to seven 7.92 mm MG 15 [Rheinmetall-Borsig_MG-15_7.92mm_MG]or MG 81 machine guns, some of them replaced or augmented by
      • 1× 20 mm MG FF [Ikaria_Werke_MG_FF-M_20mm_Cannon]cannon (central nose mount or forward ventral position)
      • 1× 13 mm MG 131 [MG_131_13mm_MG]machine gun (mounted dorsal and/or ventral rear positions)
  • Bombs:
    • up to 2,000 kg (4,409 lb) carried internally (eight 250 kg max), or:
    • up to 2,500 kg (5,512 lb) on two external racks

 

 

Heinkel He-177 (Greif)
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The Heinkel He 177 Greif (Griffin) was a long-range bomber of the Luftwaffe. The troubled aircraft was the only heavy bomber built in large numbers by Germany during World War II. Aircrews nicknamed it the Luftwaffenfeuerzeug (Luftwaffe's lighter) or the 'Flaming Coffin' due to the engines' tendency to catch fire on the early versions of the aircraft.

Earlier versions had many problems; when the problems were solved the type was successful, but could not be deployed in quantity due to Germany's deteriorating situation in the war.

The He 177 was conceived as a result of an Reichsluftfahrtministerium (RLM) requirement called the Bomber A specification which called for a bomber aircraft more advanced than the Dornier Do 19 or Junkers Ju 89 Ural-Bomber prototypes, capable of carrying a bombload of at least 1,000 kg (2,204 lb) over a range of 6,695 km (4,160 miles). The aircraft had to possess a maximum speed of about 540 km/h (335 mph) at altitude and it had to embody sufficient structural strength to enable it to undertake medium degree (later changed to 60 degree) diving attacks. In order to meet these specifications the He 177 embodied many advanced features including coupled engines with surface evaporation cooling and small remotely controlled defensive gun turrets.

An unusual feature of the aircraft was the use of twin engines in each nacelle driving a single propeller, as the components of a "power system". Siegfried Günther, chief designer of Heinkel, chose to use the Daimler-Benz DB 606, which consisted of two Daimler-Benz DB 601 engines coupled together to use a common propeller, in order to minimise drag. The two engines were coupled side by side in each nacelle and inclined inwards at the crankcases' upper surfaces, so that the inner cylinder banks were disposed almost vertically, a single gear casing connecting the two crankcases, and the two crankshaft pinions driving a single airscrew shaft gear. The insistence of this engine configuration stemmed directly from the RLM's determination that the He 177 should be capable of dive bombing. The use of only two propellers on a heavy bomber also offered a substantial reduction in drag and a marked improvement in maneuverability. Indeed, the initial prototypes and pre-production models of the bomber had an airspeed and maneuverability comparable to many heavy fighters of the time.

Both the DB 606 and 610 coupled "power systems" had A and B versions, signifying opposing rotation directions when in operation-the He 177 V1 through V3 prototypes all had the A-1 version, that rotated counterclockwise when seen from the front, used on both sides, while all later 177s, from the V4 prototype onwards through the entire production run, used one A- and one B-version of the engines, using one of the clockwise-rotation B-versions on the port-side wing.

Beset by many other technical difficulties in development and service, the plane had a troubled life. This was in part due to overly optimistic design requirements of long range, high speed, heavy bomb load, and dive bombing. Though Goering forbade Heinkel to develop a version with four separate nacelles, Heinkel nevertheless produced prototypes of the Heinkel He 177B (later renamed Heinkel He 277) which was produced in limited numbers.

Although the He 177 entered service in 1942 it was still far from operational. As an emergency measure it was used to supply the encircled 6th Armee at Stalingrad where it was determined that it could only carry about the same cargo payload as the appreciably smaller Heinkel He 111, and was useless for the evacuation of wounded troops. As a result the He 177s reverted to bombing and flak-suppression missions in support of the Wehrmacht in the vicinity of Stalingrad. Only thirteen missions were flown and seven of the He 177's crashed in flames without any action attributable to the enemy.

General characteristics

  • Crew: 5
  • Length: 22 m (72 ft 2 in)
  • Wingspan: 31.44 m (103 ft 1 in)
  • Height: 6.7 m (21 ft)
  • Wing area: 101.5 m² (1,092 ft²)
  • Empty weight: 16,800 kg (37,000 lb)
  • Loaded weight: 31,000 kg (68,340 lb)
  • Powerplant: 2× Daimler-Benz DB 610 [Daimler_Benz_DB-610_24cyl](twin DB 605) 24-cylinder liquid-cooled inline engines, 2,950 hp (2,170 kW) each

Performance

  • Maximum speed: 565 km/h (350 mph) at 6,100 m (21,000 ft)
  • Combat radius: 1.540 km (960 mi)
  • Ferry range: 5,600 km (3,200 mi)
  • Service ceiling 9,400 m (30,800 ft)
  • Wing loading: 319.9 kg/m² (65.6 lb/ft²)
  • Power/mass: 110 W/kg (0.067 hp/lb)

Armament

  • Guns:
     
    • 2 x 20 mm MG 151 [Mauser_MG-151-20_20mm_Cannon]cannon
    • 3 x MG 131 [MG_131_13mm_MG]machine gun
    • 3 x MG 81 7.92mm [Mauser_MG-81_MG]machine gun
  • Bombs: up to 7,200 kg (15,873 lb) of bombs or 3 guided missiles (Henschel Hs 293 or Fritz X)

Usual configuration:

  • 48 x 70 kg bombs (3,360 kg/7,405 lb total)
  • 10 x 500 kg bombs (5,000 kg/11,020 lb total)
  • 6 x 1000 kg bombs (6,000 kg/11,224 lb total)
  • 2 x 2500 kg bombs (5,000 kg/ 11,020 lb total)

or

  • 2 Hs 293 + 1 Hs293 remotely controlled missiles under the fuselage
  • 2 Hs 294 + 1 Hs 294 remotely controlled glide bombs under the fuselage
  • 2 PC 1400 + 1 PC 1400 gliding bomb under the fuselage
  • 2 torpedoes + 2 torpedoes under the fuselage


Junkers Ju-86
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The Junkers Ju 86 was a German monoplane bomber and civilian airliner designed in the early 1930s by Junkers. The civilian model Ju 86B could carry ten passengers; two were delivered to Swissair and five to Lufthansa. It was used by both sides in World War II. Furthermore a single civilian Ju 86Z was delivered to the Swedish AB Aerotransport.

The bomber was field tested in the Spanish Civil War, where it proved inferior to the Heinkel He 111. Four Ju 86D-1 arrived in Spain in early February 1937, but after a few sorties one of them (coded 26-1) was shot down on 23 February by Republican fighters with the loss of 3 crewmen killed and 1 captured. A replacement plane was sent from Germany, but in the summer of 1937 another D-1 was lost in an accident, and the three remaining planes were sold to the Nationalist air forces. It was again used in the 1939 invasion of Poland, but retired soon after. In January 1940 the Luftwaffe tested the prototype Ju 86P with a longer wing span, pressurized cabin, Jumo 207A1 turbocharged diesel engines, and a two-man crew. The Ju 86P could fly at heights of 12,000 m (39,000 ft) and higher on occasion, where it was felt to be safe from Allied fighters. The Westland Welkin and Yakovlev Yak-9PD were developed specifically to counter this threat.

No. 12 Squadron SAAF used Ju 86 bombers in the East African Campaign.

Satisfied with the newer version, the Luftwaffe ordered that some 40 older-model bombers be converted to Ju 86P-1 high altitude bombers and Ju 86P-2 photo reconnaissance aircraft. Those operated successfully for some years over Britain, the Soviet Union and North Africa. In August 1942, a modified Spitfire V shot one down over Egypt at some 49,000 ft (14,500 m); when two more were lost, Ju 86Ps were withdrawn from service in 1943.

Junkers developed the Ju 86R for the Luftwaffe, using larger wings and new engines capable of even higher altitudes — up to 16,000 m (52,500 ft) — but production was limited to prototypes.

General characteristics

  • Crew: 2 (pilot and radio operator)
  • Length: 16.46 m (54 ft)
  • Wingspan: 32 m (105 ft)
  • Height: 4.7 m (15 ft 5 in)
  • Wing area: 82 m² (883 ft²)
  • Empty weight: 6,700 kg (14,800 lb)
  • Max takeoff weight: 11,530 kg (25,420 lb)
  • Powerplant: Junkers Jumo 207B-3/V, [Junkers_Jumo-207B-3_6cyl_12-piston]2-stroke, 6cyl, 12 piston, diesel engines, 746 kW (1,000 hp) each

Performance

  • Maximum speed: 420 km/h (260 mph) above 9,150 m (30,000 ft)
  • Range: 1,580 km (980 mi)
  • Service ceiling 13,000 m (42,650 ft)
  • Rate of climb: 4.67 m/s (900 ft/min)
  • Wing loading: kg/m² (lb/ft²)
  • Power/mass: W/kg (hp/lb

Armament

  • Guns:
     
    • 3 x MG15 [Rheinmetall-Borsig_MG-15_7.92mm_MG]machine guns


Junkers Ju-87 (Stuka)

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The Junkers Ju 87 or Stuka (from Sturzkampfflugzeug, "dive bomber") was a two-seat (pilot and rear gunner) German ground-attack aircraft of World War II. Designed by Hermann Pohlmann, the Stuka first flew in 1935 and made its combat début in 1936 as part of the Luftwaffe's Condor Legion during the Spanish Civil War.

The aircraft was easily recognizable by its inverted gull wings, fixed spatted undercarriage and its infamous Jericho-Trompete ("Jericho Trumpet") wailing siren, becoming the propaganda symbol of German air power and the Blitzkrieg victories of 1939-1942. The Stuka's design included several innovative features, including automatic pull-up dive brakes under both wings to ensure that the plane recovered from its attack dive even if the pilot blacked out from the high acceleration. Although sturdy, accurate, and very effective, the Ju 87 was vulnerable to modern fighter aircraft, like many other dive-bombers of the war. Its flaws became apparent during the Battle of Britain - poor manoeuvrability, lack of speed and defensive armament meant that the Stuka required a fighter escort to operate effectively.

The Stuka operated with further success after the Battle of Britain, and its potency as a precision ground attack aircraft became valuable to the German war effort in the Balkans Campaign, the African and Mediterranean Theatres and the early stages of the Eastern Front campaigns where Allied fighter resistance was disorganised and in short supply. However, once the Luftwaffe had lost air superiority on all fronts the Ju 87 once again became easy targets for enemy fighter aircraft. In spite of this, and lacking a successor, the type continued to be produced until 1944. By the end of the conflict the Stuka was largely replaced by ground attack versions of the Focke-Wulf Fw 190, but some units, like Sturzkampfgeschwader 2 "Immelmann" operated the Ju 87 to the last day of the war. 5,752 Ju 87 of all versions were built between 1936 and August 1944.

Hans-Ulrich Rudel was the most notable Stuka ace and was the most highly decorated German serviceman of World War II.

The Ju 87's principal designer, Hermann Pohlmann, held the opinion that any dive-bomber design needed to be simple and robust. This led to many technical innovations, like retractable undercarriage, being removed from the design, and also led to one of the Stuka's distinctive features, its fixed and "spatted" undercarriage. Pohlmann continued to carry on developing and adding to his and Karl Plauth's ideas (Plauth was killed in a flying accident in November 1927), and produced the Ju A 48 which underwent testing on 29 September 1928.[1] The military version (designation) of the Ju A 48 was the Ju K 47.

In the early 1920s the Dessau-based Junkers Flugzeugwerke AG had concentrated upon military rather than civil aircraft, although these machines as yet had "uncranked" wings and twin tail-fin units. Because of the Versailles Treaty of 1919, which stated that Germany was not permitted to produce warplanes, the Ju K 48 was assembled and rebuilt to K 47 outside Germany by Junkers-owned subsidiaries, such as AB Flygindustri in Malmö, Sweden.

After the Nazis came to power the design was given priority. Despite initial competition from the Henschel Hs 123 the Reichsluftfahrtministerium (RLM: "Aviation Ministry"), turned to the designs of Herman Pohlmann of Junkers and co-designer of the K 47, Kark Plauth.

During the trials with the K 47 in 1932, the double vertical stabilizers were introduced to give the rear gunner a better field of fire. The main, and what was to be the most distinctive feature of the Ju 87, was its double-spar inverted gull wings.

Diving procedure

Flying at 4,600 meters (15,000 ft), the pilot located his target through a bombsight window in the cockpit floor. After opening the dive brakes, retarding his throttle, and closing the coolant flaps, he then rolled the aircraft 180°, automatically nosing the aircraft into a dive. Red tabs protruded from the upper surfaces of the wing as a visual indicator to the pilot that in case of a g induced black-out, the automatic dive recovery system would be activated. The Stuka dived at a 60 - 90 degree angle, accelerating to 600 km/h (350 mph).

When the aircraft was reasonably close to the target, a light on the contact altimeter came on to indicate the bomb-release point, usually at a minimum height of 450 m (1,500 ft). The pilot released the bomb by depressing a knob on the control column to release weapons and to initiate the automatic pull-out mechanism. An elongated U-shaped crutch located under the fuselage would swing the bomb out of the way of the propeller, and the aircraft would automatically begin a 6 g pullout.

Once the nose was above the horizon, dive brakes were retracted, the throttle was opened, and the propeller was set to climb. The pilot regained control and resumed normal flight. The coolant flaps had to be reopened quickly.

In his book Wings of the Luftwaffe, Royal Navy test pilot Eric "Winkle" Brown reported that a captured Ju 87 D-3 he test-flew after the war felt "absolutely right" diving at a 90° straight down angle, and stated that he had no doubt of the Stuka's ability in its assigned role.

General characteristics

  • Crew: 2
  • Length: 11.00 m (36 ft 1.07 in)
  • Wingspan: 13.8 m (45 ft 3.30 in)
  • Height: 4.23 m (13 ft 10.53 in)
  • Wing area: 31.90 m² (343 ft² 53.09 in²)
  • Empty weight: 3,205 kg (7,086 lb)
  • Loaded weight: 4,320 kg (9,524 lb)
  • Max takeoff weight: 5,000 kg (11,023 lb)
  • Powerplant: Junkers Jumo 211D [Junkers_Jumo_211D_V12]liquid-cooled inverted-vee V12 engine, 1200 PS (1184 hp, 883 kW)
  • Propellers: Three-bladed Junkers VS 5 propeller, 1 per engine
    • Propeller diameter: 3.4 m (11 ft 1.85 in)

Performance

  • Never exceed speed: 600 km/h (373 mph)
  • Maximum speed: 242 mph @ 13,410 ft or (390 km/h @ 4,400 m)
  • Range: 500 km (311 mi) with 500 kg (1,102 lb) bomb load
  • Service ceiling 8,200 m (26,903 ft) with 500 kg (1,102 lb) bomb load


Armament

  • Guns: 2× 7.92 mm MG 17 [Rheinmetall-Borsig_MG-17_7.92mm_MG]forward, 1× 7.92 mm MG 15 [Rheinmetall-Borsig_MG-15_7.92mm_MG]to rear
  • Bombs: Normal load = 1× 250 kg (551 lb) bomb beneath the fuselage and 2× 50 kg (110 lb) bombs underneath each wing.


Junkers Ju-88

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The Junkers Ju 88 was a World War II Luftwaffe twin-engine, multi-role aircraft. Designed by Hugo Junkers in the mid 1930s, it became one of the most versatile combat aircraft of the war. The Ju 88 suffered from a number of technical problems during the later stages of its development and early operational roles. Like a number of other Luftwaffe bombers, it was used successfully as a bomber, dive bomber, night fighter, torpedo bomber, reconnaissance aircraft, heavy fighter, and even as a flying warhead during the closing stages of conflict. Despite its protracted development, the aircraft became one of the Luftwaffe's most crucial assets. There were 15,000 Ju 88s built during World War II, more than any other twin-engined German aircraft of the period.

In October 1937 Generalluftzeugmeister Ernst Udet had ordered the development of the Ju 88 as a heavy dive-bomber. This decision was influenced by the success of the Junkers Ju 87 Stuka in this role. The Junkers development center at Dessau gave priority to the study of pull-out systems, and dive brakes. The first prototype to be tested as a dive-bomber was the Ju 88 V4 followed by the V5 and V6. These models became the planned prototype for the A-1 series. The V5 made its maiden flight on 13 April 1938, and the V6 on 28 June 1938. Both the V5 and V6 were fitted with four bladed propellers, an extra bomb bay and a central "control system". As a dive bomber, the Ju 88 was capable of pinpoint deliveries of heavy loads; however, despite all the modifications, dive bombing still proved too stressful for the airframe, and in 1943, tactics were changed so that bombs were delivered from a shallower, 45° diving angle. Aircraft and bomb sights were accordingly modified and dive brakes were removed. With an advanced Stuvi dive-bomb sight, accuracy remained very good for its time. Maximum bomb load of the A-4 was 2,500 kg, but in practice, standard bomb load was 1,500 to 2,000 kg. Junkers later used the A-4 airframe for the A-17 torpedo carrier. However the variant lacked a ventral gun position.

The standard fighter-bomber version became the Ju 88C-6, applying experience acquired with the A-4 bomber, equipped with the same Jumo 211J engines. The C-6 was used mostly as fighter-bomber and therefore assigned to bomber units. As a reaction to the increasing number of attacks on German shipping, especially on U-boats in the Bay of Biscay, from July 1942 started flying anti-shipping patrols and escort missions from bases in France.

The aircraft of V./KG 40 (which was redesignated I./Zerstörergeschwader 1 in 1943) were a significant threat to the antisubmarine aircraft and operated as escort fighters for the more vulnerable Focke-Wulf Fw 200 Condor bombers. Between July 1942 and July 1944, the Ju 88s of Kju88and ZG 1 were credited with 109 confirmed air-to air victories, at a cost of 117 losses. They were finally deployed against the Allied Invasion of Normandy in June 1944, incurring heavy losses for little effect before being disbanded on 5 August 1944.

General characteristics

  • Crew: 4
  • Length: 14.36 m (47 ft 2⅞ in)
  • Wingspan: 20.08 m (65.88 ft)
  • Height: 5.07 m (16.63 ft)
  • Wing area: 54.7 m² (587 ft²)
  • Loaded weight: 9,000 kg (20,000 lb)
  • Max takeoff weight: 14,000 kg (30,865 lb)
  • Powerplant: Junkers Jumo 211J  [Junkers_Jumo_211J_V12]liquid-cooled inverted V-12, 1,044 kW (1,420 PS, 1,401 hp) each

Performance

  • Maximum speed: 475 km/h (295 m) at 5,300 m (17,388 ft)
  • Range: 2,300 km (max internal fuel) (1,429 mi)
  • Service ceiling 8,500 m (26,900 ft)

Armament
 

  • Guns:
     
    • 3-6 machine guns, either MG 15[Rheinmetall-Borsig_MG-15_7.92mm_MG], MG 81[Mauser_MG-81_MG], MG 81Z or MG 131[MG_131_13mm_MG], with one each firing forward from both main cockpit windscreen glazing, and undernose Bola gondola, and one or two guns firing from the rear of the main cockpit (some carried one MG FF cannon [Ikaria_Werke_MG_FF-M_20mm_Cannon]in the nose)
  • Bombs: Max load 2,005kg (4,420 lb)
     
    • Ten 50kg (110 lb) bombs internally + four 250kg (551 lb) bombs externally.
    • Two 500kg (1,105 lb) externally.
    • Four 500kg (1,105lb) bombs externally.

Junkers Ju-188 (Reacher)
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The Junkers Ju 188 Rächer (Reacher) was a German World War II high-performance medium bomber from Junkers, the planned follow-on to the famed Ju 88 with better performance and payload. It was produced only in limited numbers, due both to the presence of improved versions of the Ju 88, as well as the deteriorating war condition and the resulting focus on fighter production.

The prototype Ju 88B V1, D-AUVS, flew for the first time with the 801A/B engines in early 1940. The fuselage was identical to the Ju 88 A-1, which presented a problem: with the extra power, 1,560 PS (1,539 hp, 1,147 kW), the design could now carry considerably more load than the small bomb bay could fit. An additional external shackle was then added to each wing well outside the engines, although using the rack would seriously hamper performance.

By 1942 it was becoming clear that the Ju 288 wasn't going to be ready any time soon, and at the same time the Ju 88's were increasingly at the mercy of a rapidly improving RAF and Soviet VVS. The RLM finally decided that even the small gains in performance in the Ju 88B were worth considering, and asked Junkers for a series of upgrades as the Ju 188.

The sole Ju 88 E-0 was modified with several additional guns, another MG 131 firing rearward just below the turret, one firing forward through the nose, and the twinned MG 81Z in the ventral bulge firing rearward. Two other airframes had their engines and outer wings removed to act as testbeds for water ditching, as it was planned to use the Ju 188 in long overwater flights against British shipping. A second Ju 188 test airframe was also built up from another Ju 88 A-4, this one including a larger, more trapezoidal vertical tail surface set to provide more directional control at higher altitudes, a feature also used on future Ju 88 models, such as the Ju 88G night fighters. Originally known as Ju 88 V44, this airframe was later designated Ju 188 V1.

October 1942 the program was given the go-ahead to start planning for production. A second prototype was delivered in January, which moved the outer bomb shackles to a position inboard of the engines. Both started testing the dive bombing system installed in the 88 A-4 in February. The RLM then asked for another change, allowing the aircraft to mount either the BMW 801 or Jumo 213 engines as a complete "power egg", or Kraftei, that would simply be bolted on and hooked up. Concerns about the Jumo 213, now years overdue, were offset by this engine's better altitude performance, so it made sense to delay the aircraft slightly if that meant it could switch to the 213 as soon as they became available. The second Ju 188 V1 prototype was flown in 1943.

In 1943 it was planned to upgrade the entire lineup with even more wing area and a pressurized cockpit for high-altitude work. A single basic airframe would be offered in three versions, the Ju 188J heavy fighter, Ju 188K bomber, and the Ju 188L reconnaissance version. All three did away with the under-slung gunner's compartment, leading to a cleaner nose profile, and the bomber and recce versions mounted their loads in a long pannier under the middle of the plane instead of the deeper fuselage of the G and H models.

Simpler versions of these with no defensive armament and even longer wings became the Ju 188S fighter and Ju 188T intruder. With Jumo 213 E-1 engines 2,050 PS (2,022 hp, 1,508 kW) at take-off and 1,690 PS (1,667 hp, 1,243 kW) at 9,500 m (31,400 ft), the Ju 188T could reach 700 km/h (435 mph). Operating at this altitude, the Ju 188S could carry only 800 kg of bombs.

Before any of these could start production, the entire lineup was renamed the Ju 388, the vastly improved performance warranting this change in name.

General characteristics

  • Crew: 5
  • Length: 15 m (49 ft 1 in)
  • Wingspan: 22 m (72 ft 2 in)
  • Height: 4.4 m (14 ft 7 in)
  • Wing area: 56 m² (603 ft²)
  • Empty weight: 9,900 kg (21,825 lb)
  • Loaded weight: 14,500 kg (31,967 lb)
  • Powerplant: 2× 1 BMW 801 G-2[BMW_801_14cyl_Radial], 1,250 kW (1,700 PS) each

Performance

  • Maximum speed: 499 km/h (310 mph)
  • Range: 2,190 km combat (1,360 miles)
  • Service ceiling 9,500 m (31,170 ft)
  • Wing loading: 258.9 kg/m² (53.0 lb/ft²)
  • Power/mass: 0.175 kW/kg (0.106 hp/lb)

Armament

  • Guns:
    • 1 × MG 151 20 mm [Mauser_MG-151-20_20mm_Cannon]cannon
    • 3 × MG 131 13 mm [MG_131_13mm_MG]machine gun
  • Bombs:
    • 3,000 kg (6,600 lbs)

Junkers Ju-390
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The Junkers Ju 390 was a long-range derivative of the Junkers Ju 290, and was intended to be used as a heavy transport, maritime reconnaissance aircraft, and long-range bomber. It was one of the aircraft (along with the Messerschmitt Me 264 and Focke-Wulf Ta 400) submitted for the abortive Amerika Bomber project.

Two prototypes were created by attaching an extra pair of inner-wing segments onto the wings of basic Ju 90 and Ju 290 airframes, and adding new sections to lengthen the fuselages.

The first prototype, the V1, (serial marking GH+UK), was modified from a Ju 90 V6 airframe (werke number J4918, civil registration D-AOKD from July 1940 to April 1941, then to the Luftwaffe as KH+XC, from April 1941 through April 1942, then returned to Junkerswerke and used for Ju 390 V1 construction). It made its maiden flight on October 20, 1943 and performed well, resulting in an order for 26 aircraft, to be designated Ju 390 A-1. None of these were actually built by the time that the project was cancelled (along with Ju 290 production) in mid-1944.

The second prototype, the V2 (RC+DA), was longer than the V2 because it was constructed from a Ju 290 airframe (using the fuselage of Ju 290 A1 werke number J900155).

The maritime reconnaissance and long-range bomber versions were to be designated the Ju 390 B and Ju 390 C, respectively. It has been suggested that the bomber could have carried the Messerschmitt Me 328 parasite fighter for self-defense, and some test flights are believed to have been performed by a Ju 390 prototype equipped with the anti-shipping Fritz X guided glide bomb.[

The V1 was constructed and largely assembled at Junkers' plant at Dessau, Germany, and the first test flight took place on October 20 1943. It's performance was satisfactory enough that the Air Ministry ordered 26 in addition to the two prototypes. However, the contracts for the 26 Ju 390s were cancelled in June 1944 and all work ceased in September of that year.

On November 26, 1943, the Ju 390 V1, with many other new aircraft and prototypes, was shown to Adolf Hitler at Insterburg, East Prussia.

According to former Junkers test pilot Hans-Joachim Pancherz' logbook, the Ju 390 V1 was brought to Prague immediately after it had been displayed at Insterburg, and while there took part in a number of test flights, which continued until March 1944, including tests of inflight refueling.[4]

The Ju 390 V1 was returned to Dessau in November 1944, where it was stripped of parts and finally destroyed in late April 1945 as the American Army approached.

V2

The Ju 390 V2 was assembled in Bernburg, was first flown in October 1943, and is said to have been configured for the maritime reconnaissance role. Its fuselage had been extended by 8.2 feet (2.5 m), and it was equipped with FuG 200 Hohentwiel ASV (Air to Surface Vessel) radar and defensive armament consisting of 5x 20mm cannons. Green notes different armament, specifically 4x 20mm cannon and 3x MG131 machine guns.

Test pilot Oberleutnant Eisermann recorded in his logbook that he flew the V2 prototype (RC+DA) as late as February 1944. However, Kössler and Ott state that the Ju 390 V2 was only completed during June 1944, with flight tests beginning at the end of September 1944.

A Ju 390 which may or may not have been the V2 is claimed by some to have made a test flight from Germany to Cape Town in early 1944. The sole source for the story is a speculative article which appeared in the Daily Telegraph in 1969 titled Lone Bomber Raid on New York Planned by Hitler, in which Hans Pancherz reportedly claimed to have made the flight in question. Author James P. Duffy has carried out extensive research into this claim, which has proved fruitless. Kössler and Ott make no mention of this claim either, despite having themselves interviewed Pancherz.

New York flight

The first public mention of the alleged flight of a Ju 390 to North America appeared in the November 11 1955 issue of the British magazine RAF Flying Review, of which aviation writer William Green was an editor. The magazine's editors were sceptical of the claim, which asserted that two Ju 390s had made the flight, and in March 1956 they published a letter from a reader which claimed to clarify the account. This letter stated that a single aircraft had made the flight and that it had reached a point about 12 miles (19 km) miles off the US east coast, just north of NYC.

According to Green , in June 1944 Allied Intelligence had learnt from prisoner interrogations that a Ju 390 had been delivered in January 1944 to FAGr 5 (Fernaufklärungsgruppe 5), based at Mont-de-Marsan near Bordeaux, and that it had completed a 32-hour reconnaissance flight to within 12 miles (19 km) of the US coast, north of New York City. This was, however, rejected just after the war by British authorities. Aviation historian Dr. Kenneth P. Werrell states that the story of the flight originated in two British intelligence reports from August 1944 which were based in part on the interrogation of prisoners, and titled General Report on Aircraft Engines and Aircraft Equipment; the reports claimed that the Ju 390 had taken photographs of the coast of Long Island. These photos have never been discovered.

The claimed flight was mentioned in many books following the RAF Flying Review account, including William Green's own respected Warplanes of the Second World War (1968) and Warplanes of the Third Reich (1970) but without ever citing reliable sources. Further authors then cited Green's books as their source for the claimed flight. Green himself told Kenneth P. Werrell many years later that he no longer placed much credence in the flight.

Werrell himself later examined the available data regarding the Ju 390's range and concluded that although a great circle round trip from France to St. Johns, Newfoundland was possible, adding another 2,380 miles (3,830 km) for a round trip from St. Johns to Long Island made the flight "most unlikely".

Karl Kössler and Günter Ott, in their book Die großen Dessauer: Junkers Ju 89, 90, 290, 390. Die Geschichte einer Flugzeugfamilie ("The Big Ones from Dessau...History of an Aircraft Family"), also examined the claimed flight, and thoroughly debunked the flight to Long Island. Most importantly, it was nowhere near France at the time when the flight was supposed to have taken place. According to Hans Pancherz' logbook, the Ju 390 V1 was brought to Prague on November 26, 1943. While there, it took part in a number of test flights, which continued until late March, 1944. Secondly, they also pointed out that the Ju 390 V1 prototype was unlikely to have been capable of taking off with the fuel load necessary for a flight of such duration due to strength concerns caused by its modified structure; it would have required a takeoff weight of 72 tons, while the maximum takeoff weight during its trials had been 38 tons. According to Kössler and Ott, the Ju 390 V2 could not have made the US flight either, since they indicate that it was not completed before September/October 1944.

General characteristics

  • Crew: 10
  • Length: 34.20 m (112 ft 2 in)
  • Wingspan: 50.30 m (165 ft 1 in)
  • Height: 6.89 m (22 ft 7 in)
  • Wing area: 254 m² (2,730 ft²)
  • Empty weight: 39,500 kg (87,100 lb)
  • Loaded weight: 53,112 kg (117,092 lb)
  • Max takeoff weight: 75,500 kg (166,400 lb)
  • Powerplant: BMW 801D [BMW_801D_14cyl_Radial]radial engines, 1,272 kW (1,730 hp) each

Performance

  • Maximum speed: 505 km/h (314 mph)
  • Range: 9,700 km (6,030 mi)
  • Service ceiling 6,000 m (19,700 ft)
  • Wing loading: 209 kg/m² (42.8 lb/ft²)
  • Power/mass: 0.17 kW/kg (0.10 hp/lb)

Armament

  • Guns: ** 2 × 20 mm MG 151/20 [Mauser_MG-151-20_20mm_Cannon]cannons in dorsal turrets
    • 1 × 20 mm MG 151/20 [Mauser_MG-151-20_20mm_Cannon]in tail
    • 2 × 13 mm MG 131 [MG_131_13mm_MG]machine guns at waist
    • 2 × 13 mm MG 131 in gondola
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