Ju 88 C-6 / IL-2 Sturmovik: Great Battles
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Bomber
Ju 88 C-6
History
Specifications

In 1935, the Technical Directorate of the German Air Ministry decided that the Luftwaffe needed a fast bomber instead of a multipurpose heavy fighter-bomber-reconnaissance aircraft. To this specification, Junkers developed the Ju 88, which was tested in 1936-1937, but the requirements changed again and this aircraft had to be converted into a twin-engine dive bomber. Therefore, the new bomber prototype was flown only on February 2, 1938. High speed, good maneuverability, and a heavy payload allowed it to be used for a variety of combat missions, and in 1939 the development of a heavy fighter began on this basis. The first fighters were modified from serial bombers by installing offensive armament and reducing the number of crew. They were successfully used as heavy night fighters, and in August 1941 the Air Ministry signed a contract with Junkers for the production of Ju 88 C-6 heavy fighters. The first prototype was tested in November 1940. The Ju 8 8C-6 was produced until 1944 and was continuously modernized.

The Ju 88 C-6 was a twin-engine all-metal monoplane with water-cooled Jumo 211J-1 or -2 engines with a takeoff power of 1340 hp. The aircraft was equipped with reinforced landing gear struts and larger-diameter wheels.

The first series had an offensive armament of three 20 mm cannons and three 7.92 mm machine guns, while the C-6 came with or without a pair of MG-FF/M cannons in the lower nacelle. Defensive armament varied. A pair of MG 81 machine guns or a single MG 15 or MG 131 were mounted in the rear of the cockpit. In the rear part of the nacelle, in the gondola, if there were no guns, either an MG 81Z with 1800 rounds or an MG 15 was installed. The old hatch-mounted double convex turret was replaced by a new turret. Later versions, which were used at night, did not have a nacelle under the fuselage. Later the aircraft were fitted with radar and some were also fitted with fuselage mounted 20 mm cannons firing at an angle to the horizon.

A total of 3 variants of the Ju 88 C-6 are known (note that the modification designations did not appear immediately):
  • Ju 88 C-6a heavy night fighter without radar;
  • Ju 88 C-6b heavy night fighter with FuG 202, FuG 212 or FuG 220 Lichtenstein radar. During overhauls, the passive search system FuG 227 was also installed. The night fighters were equipped with extended flame dampers on the engine exhausts;
  • The Ju 88 C-6c was characterized by the FuG 220 "Lichtenstein" SN-2 radar and later by the presence of an additional cannon battery in the so-called "schrage musik" ("jazz") installation in the central section of the fuselage. It was believed that this made it possible to hit bombers in the most vulnerable lower part of the fuselage without entering the field of fire of their defensive machine guns.

The first Ju 88 C-6 fighters, which did not have radar, entered service with night fighter formations, but despite the name, these aircraft were mainly used during the day as long-range fighters and attack aircraft. The C-6s then began to be assigned to bomber units, where specialized attack squadrons were deployed, with their primary targets being railways and vehicle convoys. With the creation of a "Sea Hunter" formation in November 1942 to operate over the Allied lines of communication in the Atlantic, another use for the C-6 became apparent. However, with the installation of radar, the Ju 88 C-6 night fighter became a crucial element of the German air defense system. In 1944, the Ju 88 assembly lines were almost completely converted to the fighter version. The deterioration of the aerodynamic qualities due to the appearance of numerous antennas affected the flight performance and controllability of the fighter, resulting in a sharp increase in operational losses.

Sources used:

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

2. "Wings of the Luftwaffe" Translation of W. Green's book "Combat Airplanes of the Third Reich" by A. Firsov, 1993.

3. materials of the site airwar.ru

Indicated stall speed in flight configuration: 185..203 km/h
Indicated stall speed in takeoff/landing configuration: 155..183 km/h
Dive speed limit: 670 km/h
Maximum load factor: 8.0 G
Stall angle of attack in flight configuration: 21.0 °
Stall angle of attack in landing configuration: 16.6 °
 
Maximum true air speed at sea level, engine mode - Climb: 427 km/h
Maximum true air speed at 2000 m, engine mode - Climb: 468 km/h
Maximum true air speed at 5300 m, engine mode - Climb: 498 km/h
 
Service ceiling: 9300 m
Climb rate at sea level: 9.2 m/s
Climb rate at 3000 m: 7.3 m/s
Climb rate at 6000 m: 5.7 m/s
 
Maximum performance turn at sea level: 26.8 s, at 250 km/h IAS.
Maximum performance turn at 3000 m: 39.4 s, at 250 km/h IAS.
 
Flight endurance at 3000 m: 4.1 h, at 300 km/h IAS.
 
Takeoff speed: 170..210 km/h
Glideslope speed: 210..220 km/h
Landing speed: 150..160 km/h
Landing angle: 9 °
 
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: 100 °C
Oil maximum temperature in engine output: 130 °C
 
Supercharger gear shift altitude: automatic 
 
Empty weight: 8315 kg
Minimum weight (no ammo, 10% fuel): 9139 kg
Standard weight: 10500 kg
Maximum takeoff weight: 13503 kg
Fuel load: 1277 kg / 1680 l
Useful load: 5188 kg
 
Forward-firing armament:
2 x 7.92mm machine gun "MG 17", 1000 rounds, 1200 rounds per minute, nose-mounted
7.92mm machine gun "MG 17", 800 rounds, 1200 rounds per minute, nose-mounted
3 x 20mm gun "MG FF", 120 rounds, 540 rounds per minute, nose-mounted
20mm gun "MG 151/20", 350 rounds, 700 rounds per minute, nose-mounted (modification)
 
Defensive armament:
Top: 7.92mm machine gun "MG 81", 1000 rounds, 1600 rounds per minute
Top: 13.0mm machine gun "MG 131", 500 rounds, 900 rounds per minute (modification)
 
Bombs:
Up to 10 x 55 kg general purpose bombs "SC 50"
Up to 2 x 249 kg general purpose bombs "SC 250"
Up to 2 x 500 kg general purpose bombs "SC 500"
Up to 2 x 1090 kg general purpose bombs "SC 1000"
 
Length: 14.3 m
Wingspan: 20.02 m
Wing surface: 52.7 m²
 
Combat debut: November 1942
 
Operation features:
- Each engine has a two-stage mechanical supercharger with an automatic switch system that switches gears depending 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.
- Propellers have a feathering system which should be activated in case of engine damage to reduce drag of the propeller in auto-rotation.
- Water and oil radiators shutters are joint with engine cowl outlet shutters and manually operated. Ground personnel may install additional fixed shutters on the intake of the oil radiators in cold weather to prevent freezing of the oil.
- The aircraft has a fuel gauge which shows remaining fuel in fuel tanks depending on switch position. In game the fuel indicator switch changes by pressing (RShift+I).
- The aircraft has trimmers for all flight-controls: pitch, roll and yaw.
- The aircraft has hydraulic-actuated landing flaps with three fixed positions: retracted, takeoff (25°) and landing (50°). Flap indicator lights are located on left panel.
- 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 flaps indicator lights.
- The aircraft is also equipped with differential ailerons which are lowered in synch with the flaps.
- Lowering the landing gear takes a long time, for this reason it is necessary to extend the landing gear well before final landing approach.
- The aircraft tailwheel rotates freely and does not have a lock. For this reason, it is necessary to confidently and accurately operate the rudder pedals during the 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 dedicated fuel gauges for left and right fuel tank groups and there is a switch between the internal and external fuel tank group indicator. In game the fuel indicator switch changes by itself during horizontal flight every 10 seconds. Also, the airplane has low fuel warning lights (180 liters) for the internal tanks.
- Aiming line of forward-firing armament is set at an elevation angle of -4.5 degrees.
- The aircraft is equipped with an automatic bomb salvo controller, it allows you to switch between the bomb racks to be released (internal or external) and to switch between different salvo quantities. There is also a controller for a drop delay between each bomb in the salvo.
 
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 cowl flap control handle: close
- recommended position of the prop pitch control handle: heavy
- recommended position of the throttle lever: 10%
 
2. Recommended mixture control lever positions for various flight modes: auto mixture control
 
3. Recommended positions of the cowl flap control handle for various flight modes:
- takeoff: open 100%
- climb: open 100%
- cruise flight: open 20% (in winter conditions - close if necessary)
- combat: open 50% (in winter conditions - close if necessary)
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 10.5 l/min
- Combat engine mode: 16.0 l/min
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