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===The diving sequence===
===The diving sequence===
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 and slowing his throttle, he then rolls 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 incase of a [[Acceleration due to gravity|''g'']] induced black-out, the automatic dive recovery system was activated.
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 and slowing his throttle, 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 [[Acceleration due to gravity|''g'']] induced black-out, the automatic dive recovery system would be activated.


The Stuka dove at 60 - 90 degree angle, accelerating to 600 km/h (350 mph).
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. A clutch located under the fuselage would swing the bomb out of the way of the propellor, and the aircraft would automatically begin a 6 [[Acceleration due to gravity|''g'']] pullout.
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. A clutch located under the fuselage would swing the bomb out of the way of the propellor, and the aircraft would automatically begin a 6 [[Acceleration due to gravity|''g'']] pullout.

Revision as of 06:05, 21 August 2006

"Stuka" redirects here. For the artillery piece nicknamed the "Walking Stuka", see Wurfrahmen 40.
File:Junkers Ju87.jpg
Junkers Ju 87 Dive-Bombers

The Junkers Ju 87 or Stuka was the best known Sturzkampfflugzeug (German dive bomber) in World War II, instantly recognisable by its inverted gull wings, fixed undercarriage and infamous wailing siren.

The Stuka's design featured some innovative features, including an automatic pull-up system to ensure that the plane recovered from its attack dive even if the pilot blacked out from the high acceleration, and wind-powered sirens on the wheel covers that wailed during dives to frighten its victims. These were named "Trumpets of Jericho" by Junkers and were a form of psychological warfare. Its rugged fixed undercarriage allowed it to land and take-off from improvised airstrips close to the battlefront, giving close support to the advancing German forces.

Although sturdy, accurate, and very effective, the Stuka suffered from low speed and maneuverabilty, with little defensive armament, making it highly vulnerable to enemy fighters. The Germans learned in the Battle of Britain that air superiority must be obtained before ground attack aircraft could be effectively used. After the Battle of Britain, the Stuka was little used in western Europe, but it remained effective further south where Allied fighters were in short supply (notably in the attacks on Crete and Malta), and was used in vast numbers on the Eastern Front, although the steady rise in Soviet airpower as the war progressed meant that Stuka squadrons suffered very heavy losses.

More than six thousand Ju 87 were built between 1936 and August 1944.

It was a Ju 87 that achieved the first Axis air victory during World War II.[1]

Hans-Ulrich Rudel was the most notable Stuka ace, and in fact the most highly decorated German soldier of the war.

General Characteristics

Models not listed include the Ju 87C naval derivative of the Ju 87B, intended for use on the aircraft carrier Graf Zeppelin; the Ju 87E naval derivative of the Ju 87D; the Ju 87R long-range version of the Ju 87B; the Ju 87H disarmed versions of the equivalent D-models for use as trainers; the Ju 87K export models; the Ju 87D-5/D-6 with increased wing span.

Ju 87A Ju 87B Ju 87D Ju 87G
Production 1936-1938 1938-1941 1941-1944 refitted Ju 87D
Role ground attack ground attack ground attack anti-tank
Length 10.8 m 11.1 m 11.1 m 11.1 m
Wingspan 13.8 m 13.8 m 13.8 m 13.8 m
Height 3.9 m 3.9 m 3.9 m 3.9 m
Wing area 31.90 m² 31.90 m² 31.90 m² 31.90 m²
Empty weight 2273 kg 2760 kg 2810 kg 3600 kg
Maximum weight 3324 kg 4400 kg 5720 kg 5100 kg
Engine Junkers Jumo 210D Junkers Jumo 211Da Junkers Jumo 211J Junkers Jumo 211J
Maximum Power 720 hp 1200 hp 1410 hp 1410 hp
Maximum Power 530 kW 883 kW 1037 kW 1037 kW
Maximum speed 310 km/h 340 km/h 354 km/h 344 km/h
Dive speed 550 km/h 600 km/h 600 km/h
Range with bombs 800 km 600 km 1165 km 1000 km
Ceiling 9430 m 8100 m 9000 m 7500 m
Climb 3000 m in 8.8 min 3000 m in 14 min 3000 m in 13.6 min
Forward guns 1×7.92 mm MG 17 2×7.92 mm MG 17 2×7.92 mm MG 17 2×7.92 mm MG 17
2×37 mm BK 37
Rear guns 1×7.92 mm MG 15 1×7.92 mm MG 15 1×7.92 mm MG 81Z
(twin MG 81)
1×7.92 mm MG 81Z
(twin MG 81)
Maximum bombs 250 kg 500 kg 1800 kg none
Typical bombs 1×250 kg 1×250 kg
+ 4×50 kg
1×500/1000 kg
+ 4×50 kg
none
  • The Ju 87A was able to carry a single 500 kg bomb but only without the rear gunner and at short ranges.
  • The Ju 87B might have been able to carry a single 1000 kg bomb but only without rear gunner and at short ranges.
  • The Ju 87D was able to carry its maximum bomb load only at short ranges.
  • The Ju 87D-5 increased wing span to 15.00 m and replaced the MG 17 with two MG 151/20 cannons to improve ground attack capability.

Other designs

The concept of dive bombing became so popular among the leadership of the Luftwaffe, that it became almost obligatory in new aircraft designs. Later bomber models like the Junkers Ju 88 and the Dornier Do 217 were fitted for dive bombing. Even the giant Heinkel He 177 bomber was initially supposed to have dive bombing capabilities — a requirement that contributed much to the failure of the design.

The diving sequence

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 and slowing his throttle, 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. A clutch located under the fuselage would swing the bomb out of the way of the propellor, 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 remaining bombs under the wings were used for other targets.

Surviving Aircraft

Two intact Ju 87s survive. A Ju 87G-2, captured by British troops in Germany in 1945, is displayed in the RAF Museum in London. The Chicago Museum of Science and Industry has a Ju 87 R-2/Trop, this was captured in Libya 1941 and subsequently sent to the US. The Deutsches Technikmuseum in Berlin has the wreckage of two complete aircraft that were recovered from separate crash sites near Murmansk in 1990 and 1994. The Sinsheim Auto & Technik Museum displays the remains of an aircraft that crashed near Saint-Tropez in 1944 and was raised from the sea-bed in 1989.

Operators

References

  1. ^ The first Axis air victory in World War II, was achieved on September 1 at dawn, by a German Ju 87 which shot down a Polish PZL P.11c fighter aircraft of Capt. Mieczysław Medwecki.

Related development Ju 187 Ju 287 Related lists List of military aircraft of Germany - List of bomber aircraft