Ju 87 D-3 / IL-2 Sturmovik: Great Battles
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Sturmovik
Ju 87 D-3
History
Specifications

In 1933, the Germans purchased 2 Helldiver dive bombers from the United States, whose tests showed high efficiency in dive bombing. In 1935, the basic requirements for a dive bomber ("Stuka" is an abbreviation of the German term Sturzkampfflugzeug - dive bomber) were determined. The Luftwaffe produced an archaic-looking Ju 87 aircraft with a fixed landing gear enclosed in fairings and mounted on a wing with a characteristic bend. The plane was successfully used in the Polish and French campaigns, but the units armed with these planes suffered relatively heavy losses due to the low speed, weak armament, and protection of the aircraft. Therefore, in 1940, the Junkers company began to develop a new modification of the Ju 87 that would be better suited for attacks on well-protected and fortified targets. The new model was called the Ju 8 D ("Dora"). The more powerful Jumo 211 engine and significantly improved aerodynamics of the aircraft made it possible to strengthen the armor, install more effective small arms, and increase the bomb load, which now included armor-piercing bombs. The vulnerability of the Ju 87 as a bomber, unable to defend itself against enemy fighters and poorly protected against antiaircraft fire, led to a complete modernization of the aircraft and a change in its primary purpose. As a result, Junkers launched the Ju 87 D-3, the first attack aircraft in the Ju 87 family.

The Ju 87 D-3 modification went into production at the end of 1942. The Jumo 211J-1 engine installed on it developed 1420 hp at takeoff and 1410 hp at an altitude of 4300 m. The cockpit, engine, and radiators of the plane were armored, the pilot was provided with a canopy made of two-inch armored glass, 8 mm chrome-nickel steel plates were installed on the cockpit sides, additional armor plates were mounted on the turret and around the gunner's head, and on some planes even the movable canopy doors were armored. The new GSL-K81Z gun mount had increased sighting angles, but gunners found the new cockpit cramped and uncomfortable. There was also an additional 5 mm armor plate under the oil cooler and armor plates covering the fuel tanks in the center section from the front and sides. However, the armor of the Ju 87 D protected the crew and vital systems of the aircraft only against armor-piercing bullets of conventional caliber, provided that the shooting was carried out at a distance of up to 400 m and the angle of contact with the armor did not exceed 15-20 degrees.

On the wings, the rubber "anti-skid" track was replaced by a corrugated metal strip. The air brakes were retained.

The small arms did not change and still consisted of three 7.92 mm machine guns. The main weapons of the D-3 were containers filled with 92 SD 2 fragmentation bombs of 2 kg each. Bombs of 500 and 250 kg could also be carried.

Almost all of the 1,559 Ju 87 D-3s produced went to the Eastern Front. As the war progressed, the use of the "Stukas" on both the Eastern and Western fronts became increasingly limited due to their high vulnerability, so that by the end of the war they were mainly used in special "night" formations, and in October 1944 production of all Ju 87 models was stopped.

1. W. Creen “The Warplanes of the Third Reich”, Galahad Books, 1986

2. “Wings of the Luftwaffe” Translation of V. Green’s book “Combat Aircraft of the Third Reich” by A. Firsov, 1993

3. A. Demin. “Junkers Ju 87 dive bomber” Magazine “Aviation and Cosmonautics”, No. 6-10 2001

4. Materials from the site airwar.ru

Indicated stall speed in flight configuration: 137..176 km/h
Indicated stall speed in takeoff/landing configuration: 123..155 km/h
 
Dive speed limit: 650 km/h
Maximum load factor: 9 G
Stall angle of attack in flight configuration: 19.9 °
Stall angle of attack in landing configuration: 18 °
 
Maximum true air speed at sea level, engine mode - Climb: 367 km/h
Maximum true air speed at 2000 m, engine mode - Climb: 389 km/h
Maximum true air speed at 6000 m, engine mode - Climb: 422 km/h
 
Service ceiling: 7000 m
Climb rate at sea level: 8 m/s
Climb rate at 3000 m: 7 m/s
Climb rate at 6000 m: 2.5 m/s
 
Maximum performance turn at sea level: 22.2 s, at 230 km/h IAS.
Maximum performance turn at 3000 m: 31.3 s, at 230 km/h IAS.
 
Flight endurance at 3000 m: 3.4 h, at 300 km/h IAS.
 
Takeoff speed: 140..170 km/h
Glideslope speed: 180..195 km/h
Landing speed: 125..145 km/h
Landing angle: 11 °
 
Note 1: the data provided is for international standard atmosphere (ISA).
Note 2: flight performance ranges are given for possible aircraft mass ranges.
Note 3: maximum speeds, climb rates and turn times are given for standard aircraft mass.
Note 4: climb rates are given for Climb power, turn times are given for Take-off power.
 
Engine:
Model: Jumo-211J
Maximum power in Take-off mode at sea level: 1420 HP
Maximum power in Climb mode at sea level: 1190 HP
Maximum power in Climb mode at 1500 m: 1260 HP
Maximum power in Climb mode at 4900 m: 1180 HP
 
Engine modes:
Nominal (unlimited time): 2250 RPM, 1.15 ata
Climb power (up to 30 minutes): 2400 RPM, 1.25 ata
Take-off power (up to 1 minute): 2600 RPM, 1.42 ata
 
Water rated temperature in engine output: 80 °C
Water maximum temperature in engine output: 110 °C
Oil rated temperature in engine output: 90 °C
Oil maximum temperature in engine output: 105 °C
 
Supercharger gear shift altitude: automatic 
 
Empty weight: 3930 kg
Minimum weight (no ammo, 10% fuel): 4250 kg
Standard weight: 4835 kg
Maximum takeoff weight: 6684 kg
Fuel load: 626 kg / 840 l
Useful load: 2754 kg
 
Forward-firing armament:
2 x 7.92mm machine gun "MG 17", 1000 rounds, 1200 rounds per minute, nose-mounted
12 x 7.92mm machine gun "MG 81", 250 rounds, 1600 rounds per minute, wing-mounted (modification)
2 x 37mm gun "BK 3.7", 12 rounds, 160 rounds per minute, wing-mounted (modification)
 
Defensive armament:
Backward: 2 x 7.92mm machine gun "MG 81", 500 rounds, 1600 rounds per minute
 
Bombs:
Up to 4 x 66 kg general purpose bomb "SD 70"
Up to 3 x 249 kg general purpose bombs "SC 250"
500 kg general purpose bomb "SC 500"
1090 kg general purpose bomb "SC 1000"
1780 kg general purpose bomb "SC 1800"
 
Length: 11 m
Wingspan: 13.8 m
Wing surface: 31.9 m²
 
Combat debut: March 1942
 
Operation features:
- The engine has a two-stage mechanical supercharger with an automatic switch system that switches gears depending on altitude and engine revolutions. It can also be manually switched to first gear.
- Engine mixture control is automatic.
- Engine RPM has an automatic governor and it is maintained at the required RPM corresponding to the governor control lever position. The governor automatically controls the propeller pitch to maintain the required RPM.
- Water and oil radiator shutters are controlled manually.
- The aircraft has only the pitch and yaw flight-control trimmers.
- The aircraft has fence-type airbrakes which are located under the wing and used to slow the descent during steep dive bombing.
- The aircraft has hydraulic-actuated landing flaps with three fixed positions: retracted, takeoff (25°) and landing (40°). Flap indicator lights are located on left panel near the throttle.
- The aircraft is also equipped with differential ailerons which are lowered in synch with the flaps.
- The aircraft has an automatically controlled horizontal stabilizer. An automatic control system adjusts the stabilizer angle depending on the extended angle of the landing flaps. The stabilizer control lamps are located near the throttle lever.
- The aircraft has a manual tailwheel lock. Wheel should be locked when taxiing straight for a long distance and before takeoff and landing.
- The aircraft has independent left and right hydraulic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- The aircraft has a fuel gauge which shows remaining fuel in left and right fuel tanks depending on switch position. In game the fuel indicator switch changes by pressing (RShift+I). Also, the airplane has indicator lights for full internal tanks and a low fuel warning light (160 liters) for each tank.
- It is impossible to open or close the canopy at high speed due to strong airflow. When the canopy is open, it is impossible to use rear gun because it is linked to canopy. The canopy has an emergency release system for bailouts.
- The aircraft has a window in the cockpit floor which can be opened by the bomb bay door command.
- The aircraft is equipped with a salvo controller, it allows the pilot to choose which bomb racks to use (central, left and right wing) and to switch the bomb salvo (single drop or all bombs on the rack).
- The gunsight has a sliding sun-filter.
- The aircraft is equipped with dive system. When the dive system is engaged, the plane enters a dive when the air brakes are extended and will recover from the dive either by pressing the bomb drop button or when the air brakes are retracted. The dive system controls are separate: the trimmer tab on the right elevator is controlled by the dive system while the pilot controls the trimmer tab on the left elevator. Therefore the pilot input and dive system input of the trimmers are independent, and when the dive system is in operation, there is no indication of a trimmer position change in the technochat.
 
Basic data and recommended positions of the aircraft controls:
1. Starting the engine:
- recommended position of the mixture control lever: auto mixture control
- recommended position of the radiators control handle: close
- recommended position of the prop pitch control handle: light
- recommended position of the throttle lever: 0%
- before taxiing, you must unlock the tailwheel
 
2. Recommended mixture control lever positions for various flight modes: auto mixture control
 
3.1 Recommended positions of the oil radiator control handle for various flight modes:
- takeoff: open 50%
- climb: open 100%
- cruise flight: open 40% (in winter conditions - open 20%)
- combat: open 50%
 
3.2 Recommended positions of the water radiator control handle for various flight modes:
- takeoff: open 50%
- climb: open 100%
- cruise flight: open 40% (in winter conditions - close if necessary)
- combat: open 50%
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 3.7 l/min
- Combat engine mode: 6.8 l/min
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