I-16 type 24 / IL-2 Sturmovik: Great Battles
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Fighter
I-16 type 24
History
Specifications

Polikarpov's most famous fighter appeared in 1933. This aircraft was designed as a new generation high-speed monoplane, which at the same time was supposed to have high combat maneuverability. Its small size made it easy to fly, but its rearward orientation and dimensions made it unstable in flight, requiring more attention from the pilot — the aircraft responded to the slightest movement of the stick — but pilots who could fly the I-16 could usually fly other aircraft with ease. The I-16 became one of the most popular fighters of the pre-war Soviet Air Force and was used in all wars and armed conflicts in which the USSR participated. By 1939, the aircraft had practically exhausted the possibilities of modernization, which was particularly evident in the events of the final period of the Spanish Civil War, but it was well mastered by both industry and pilots, so another modification of the M-62 engine was developed at the Perm engine plant No. 19, which received the designation M-63.

The M-63 developed 1100 hp. (for the M-62 - 1000 hp) with only 5 kg more weight. This engine was chosen to power a modified I-16 which became known as the I-16 Type 24.

The I-16 had a mixed construction. The fuselage was made of wood with a frame made of four pine spars, eleven frames, and stringers. The skin was veneer laminated and consisted of two pieces attached to the frame with glue and nails. The finished fuselage was covered with fabric, carefully putty-wrapped, and sanded. The two-spar wing consisted of a center section and a pair of removable sections. The wing tips were covered with duralumin sheeting, and the entire wing was covered with percale. On the Type 24, the top of the wing was covered with plywood. Large ailerons occupied the entire trailing edge of the wings. The tail unit was metal with a fabric covering. The rudders, like the ailerons, had tubular spars.

The landing gear was retractable, of the pyramid type: the retraction system was manual, driven by a winch located on the right side of the cabin, and turned out to be very complex and unreliable due to the abundance of cables, rollers, clamps, and other elements.

The armament consisted of two wing-mounted and two propeller-synchronized 7.62 mm ShKAS machine guns.

State tests of the I-16 Type 24, which began in the first half of 1940, showed that there was no significant improvement in flight characteristics compared to the I-16 Type 18 with the M-62 engine, and the maneuverability of the new modification even decreased somewhat. The increased weight of the reinforced wing and fuselage structure "ate up" the additional power gained by installing the M-63 engine. A total of 964 I-16 Type 24 aircraft were produced.

At dawn on June 22, 1941, Germany repeated its invasion scenario, which had been executed many times before in Europe: 66 airfields, where the main air forces covering the border were located, were attacked almost simultaneously. By the evening, the losses of the air force amounted to about 1,200 aircraft, but the Soviet pilots resisted skillfully and stubbornly, despite heavy losses. Suddenly, the I-16, flown by a skilled pilot, proved to be a dangerous opponent. For example, in 1942, the number of combat losses of the I-16 was lower than that of other fighters in service with the Soviet Air Force. The German pilots who fought on the Eastern Front did not consider the I-16 easy prey: although they could almost always impose the initiative on the "donkey" pilot in an air battle, they tried to avoid a maneuverable battle with a Russian veteran. Interestingly, the 1st Guards Fighter Aviation Regiment received its title in December 1941, fighting on I-16 Type 24 aircraft.

Used sources:

1. V. Shavrov, “History of aircraft designs in the USSR until 1938”, 2002

2. S. Ivanov, “Polikarpov Fighters Part 2.” Magazine "War in the Air", No. 137, 2005

3. Materials from the site airwar.ru

Indicated stall speed in flight configuration: 143..164 km/h
Indicated stall speed in takeoff/landing configuration: 142..163 km/h
Dive speed limit: 620 km/h
Maximum load factor: 12 G
Stall angle of attack in flight configuration: 17.6 °
Stall angle of attack in landing configuration: 15 °
 
Maximum true air speed at sea level, engine mode - Boosted: 448 km/h
Maximum true air speed at 1800 m, engine mode - Nominal: 460 km/h
Maximum true air speed at 4500 m, engine mode - Nominal: 490 km/h
 
Service ceiling: 10500 m
Climb rate at sea level: 16.7 m/s
Climb rate at 3000 m: 13.8 m/s
Climb rate at 6000 m: 8.8 m/s
 
Maximum performance turn at sea level: 19.0 s, at 230 km/h IAS.
Maximum performance turn at 3000 m: 25.3 s, at 230 km/h IAS.
 
Flight endurance at 3000 m: 0.9 h, at 350 km/h IAS.
 
Takeoff speed: 145..175 km/h
Glideslope speed: 185..195 km/h
Landing speed: 135..145 km/h
Landing angle: 15.3 °
 
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 Boosted power.
 
Engine:
Model: M-63
Maximum power in Boosted mode at sea level: 1100 HP
Maximum power in Nominal mode at sea level: 930 HP
Maximum power in Nominal mode at 1800 m: 1000 HP
Maximum power in Nominal mode at 4500 m: 900 HP
 
Engine modes:
Nominal (unlimited time): 2200 RPM, 915 mm Hg
Boosted power (up to 5 minutes): 2300 RPM, 1065 mm Hg
 
Oil rated temperature in engine output: 55..90 °C
Oil maximum temperature in engine output: 125 °C
Cylinder head rated temperature: 120..200 °C
Cylinder head maximum temperature: 205 °C
 
Supercharger gear shift altitude: 3000 m
 
Empty weight: 1501 kg
Minimum weight (no ammo, 10% fuel): 1633 kg
Standard weight: 1878 kg
Maximum takeoff weight: 2146 kg
Fuel load: 191 kg / 260 l
Useful load: 645 kg
 
Forward-firing armament:
2 x 7.62mm machine gun "ShKAS", 500 rounds, 1800 rounds per minute, synchronized
2 x 7.62mm machine gun "ShKAS", 900 rounds, 1800 rounds per minute, wing-mounted
2 x 20mm gun "SsVAK", 90 rounds, 800 rounds per minute, wing-mounted (modification)
 
Bombs:
2 x 50 kg general purpose bombs "FAB-50sv"
2 x 104 kg general purpose bombs "FAB-100M"
 
Rockets:
Up to 6 x 7 kg rockets "ROS-82", HE payload mass 2.52 kg
 
Length: 6.04 m
Wingspan: 9 m
Wing surface: 14.54 m²
 
Combat debut: June 1941
 
Operation features:
- The engine has a boost mode. To set boost mode it is necessary to push the boost lever fully forward and increase the engine to 2300 RPM.
- The engine has a two-stage mechanical supercharger which should be manually shifted at 3000m altitude.
- Engine mixture control is automatic when the mixture lever is set to maximum. It is possible to manually lean the mixture by moving the mixture control to less than maximum. This also reduces fuel consumption during flight.
- 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.
- Oil radiator shutter and air cooling intake shutters control is manual.
- The aircraft has no flight-control trimmers. Airplane is equipped with bendable trim tabs that can be set pre-flight by ground personnel.
- The aircraft has a manual system for landing flaps and gear, for this reason it is necessary to extend landing flaps and gear before final approach. Landing flaps can be extended to any angle up to 53°.
- The aircraft has a tailwheel control mechanism which is linked to rudder pedals. Because of this, it is necessary to avoid of large rudder pedal inputs when moving at high speed on the ground.
- The aircraft has independent left and right mechanical wheel brakes. To brake it is necessary to push upper part of the rudder pedal.
- The aircraft has a hydrostatic fuel gauge which shows total fuel remaining only when manual sucker lever is pushed in. In game this happens by pressing (RShift+I by default).
- Cockpit has side-doors which should be closed before takeoff to prevent damage.
- When bombs are installed there is a salvo controller, it has two release modes: single drop or drop two in a salvo.
- When rockets are installed there is a salvo controller, it has three launch modes: single fire, fire two in a salvo or fire four in a salvo.
- The gunsight has a sliding sun-filter. There is also a back-up folding mechanical sight which can be used if main sight is damaged.
 
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: 50%
- recommended position of the radiator control handle: 50%
- recommended position of the prop pitch control handle: light 90%
- recommended position of the throttle lever: 5%
 
2. Recommended mixture control lever positions for various flight modes: auto mixture control
 
3.1 Recommended positions of cowl flaps for various flight modes:
- takeoff: open 50%
- climb: open 100%
- cruise flight: open 30% (in winter conditions - close to 15% if necessary)
- combat: open 70%
 
3.2 Recommended positions of the oil radiator control handle for various flight modes:
- takeoff: open 50%
- climb: open 100%
- cruise flight: open 60%
- combat: open 100%
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 6.4 l/min
- Combat engine mode: 6.8 l/min
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