Hs 129 B-2 / IL-2 Sturmovik: Great Battles
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Sturmovik
Hs 129 B-2
History
Specifications

In April 1939, the first example of an armored attack aircraft from the Luftwaffe company "Henschel" took to the skies. Based on the experience of the Spanish Civil War, the German Air Ministry concluded in 1937 that it was advisable to have a special armored fighter for fire support. This aircraft would fight with armored vehicles and help break through the enemy's defenses. The development and testing of the aircraft were delayed due to numerous design flaws and a lack of suitable engines, as the Argus As410 used had too little power. In 1940, however, it became possible to install more powerful French Gnome-Rhone 14M 04/05 engines, which became available after the occupation of France. In addition, combat operations during the French and Polish campaigns proved the Ju 87 to be a complete failure as an attack aircraft. The Hs 129 B modification with these engines was produced in 1941. In May 1942, the Hs 129 B-2 modification was introduced, differing only in an improved fuel system.

The Hs 129 B-2 was a twin-engine, all-metal monoplane without external struts and with armored cockpit and engines. The Gnome-Rhone 14M 04/05 engines developed 700 hp at takeoff and 660 hp at 4000 meters. The engines and oil coolers were protected by 5 mm armor. The armored cockpit was welded from steel plates with thicknesses from 6 (top and sides) to 12 millimeters (bottom, front, and rear walls). The front armored glass was 75 millimeters thick. The cockpit was so small that some of the instruments were moved to the inside of the nacelles, and the sight was mounted in an armored housing outside in front of the armored glass. The control stick was also very short due to the pilot's low seating position, requiring a lot of effort from the pilot. The standard armament consisted of two 7.92 mm MG 17 machine guns and two 20 mm MG 151/20 cannons.

The following field conversion kits were available:
  • B-2 /R1: 2 ETC 50 racks under the wings and 4 ETC 50 racks under the fuselage, allowing to carry up to 300 kg of bombs or 6 AB 24 containers (each with 24 anti-personnel mines);
  • B-2 /R2: 30 mm MK 101 cannon (MK 103 from mid-1943) with 100 rounds of ammunition mounted under the fuselage;
  • B-2 /R3: with 37 mm BK 3.7 cannon (with 12 rounds of ammunition) under the fuselage. The MG 17 machine guns were removed.

A total of about 780 Hs 129 B-2s were built. The aircraft was mainly used on the Eastern Front as part of the so-called "antitank squadrons." It fought in small numbers in North Africa. It was delivered to Romania (62 aircraft) and Hungary (4 aircraft). The use of the Hs 129 on the fronts could not have a significant impact on the course of hostilities, unlike the use of the Soviet Il-2 attack aircraft, due to design flaws: difficult control, low speed, unreliable and poorly armored engines, lack of protective armament at the rear. German pilots were more than critical of their Henschel. One German pilot admitted after the war that the performance of the machine was so poor and flying it so dangerous that he still had nightmares about it.

It is interesting to note that at the end of the war, the Romanian Air Force used the plane in battles against German troops. At the same time, they lost 4 planes: 1 from anti-aircraft fire, 1 in an accident, and 2 missing.

Used sources:

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. "Luftwaffe Flying Tank" Aviafan Magazine, 1995.

4. Materials from the site airwar.ru

Indicated stall speed in flight configuration: 143..159 km/h
Indicated stall speed in takeoff/landing configuration: 136..150 km/h
Dive speed limit: 670 km/h
Maximum load factor: 9 G
Stall angle of attack in flight configuration: 20.0 °
Stall angle of attack in landing configuration: 18.0 °
 
Maximum true air speed at sea level, engine mode - Combat: 349 km/h
Maximum true air speed at 3000 m, engine mode - Combat: 396 km/h
 
Service ceiling: 7000 m
Climb rate at sea level: 8.4 m/s
Climb rate at 3000 m: 8.1 m/s
Climb rate at 6000 m: 2.6 m/s
 
Maximum performance turn at sea level: 30.0 s, at 255 km/h IAS.
Maximum performance turn at 3000 m: 46.0 s, at 270 km/h IAS.
 
Flight endurance at 3000 m: 2.1 h, at 300 km/h IAS.
 
Takeoff speed: 145..155 km/h
Glideslope speed: 180..200 km/h
Landing speed: 135..145 km/h
Landing angle: 10.6 °
 
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 and turn times are given for Combat power.
 
Engine:
Model: Gnome-Rhone 14 M
Maximum power in Take-off mode at sea level: 700 HP
Maximum power in Combat mode at sea level: 580 HP
Maximum power in Combat mode at 4000 m: 650 HP
 
Engine modes:
Nominal (unlimited time): 2350 RPM, 1.1 ata
Combat power (up to 30 minutes): 2750 RPM, 1.25 ata
Take-off power (up to 1 minute): 3030 RPM, 1.5 ata
 
Oil rated temperature in engine intake: 60..75 °C
Oil maximum temperature in engine intake: 125 °C
 
Supercharger gear shift altitude: single gear
 
Empty weight: 3992 kg
Minimum weight (no ammo, 10% fuel): 4200 kg
Standart weight: 4756 kg
Maximum takeoff weight: 5170 kg
Fuel load: 451 kg / 610 l
Useful load: 1178 kg
 
Forward-firing armament:
2 x 7.92mm machine gun "MG 17", 1000 rounds, 1200 rounds per minute, nose-mounted
2 x 15mm gun "MG 151/15", 250 rounds, 700 rounds per minute, nose-mounted
2 x 20mm gun "MG 151/20", 250 rounds, 700 rounds per minute, nose-mounted (modification)
4 x 7.92mm machine gun "MG 17", 1000 rounds, 1200 rounds per minute, underbelly (modification)
30mm gun "MK 101", 30 rounds, 250 rounds per minute, underbelly (modification)
30mm gun "MK 103", 80 rounds, 400 rounds per minute, underbelly (modification)
 
Bombs:
Up to 6 x 55 kg general purpose bombs "SC 50"
249 kg general purpose bombs "SC 250"
 
Length: 9.7 m
Wingspan: 14.2 m
Wing surface: 28.9 m²
 
Combat debut: May 1942
 
Operation features:
- Controlling the propellers RPM is possible only in the manual mode by changing the propeller pitch. The automatic mode keeps the RPM at 2750.
- The engine control lever allows setting the pressure up to the combat mode (1.25 ATA).
- To switch the engines to the take-off mode, move the boost lever to 1.5 ATA position and set the propellers to 3030 RPM.
- Engine mixture control is automatic. Leaning the mixture manually reduces the fuel consumption during flight.
- The oil radiator shutters are controlled automatically and do not have a manual mode.
- The propellers have a feathering system which should be activated in case of engine damage to reduce drag of the propeller in auto-rotation.
- The aircraft has only pitch and yaw flight-control trimmers.
- The aircraft has independent left and right hydraulic wheel brake controls. To apply either brake push the upper part of the rudder pedal.
- Landing flaps have a hydraulic actuator and they can be extended to any angle up to 40° or to the fixed take-off position.
- The 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 fuel gauges are positioned directly on the engine nacelles and show only the amount of fuel remaining in the wing tanks (the fuel remaining in the central fuel tank is not indicated).
- The aircraft isn't equipped with an oxygen supply system, so flying above 4000 meters is forbidden.
- The aircraft is equipped with an electric bomb release controller that allows dropping the bombs only one by one.
- The gunsight has a sliding sun-filter.
 
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 oil radiator control handle: auto radiator control
- recommended position of the prop pitch control handle: auto prop pitch control
- 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 radiator control handle for various flight modes: auto radiator control
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 4.5 l/min
- Combat engine mode: 7.4 l/min
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