Spitfire Mk.XIV / IL-2 Sturmovik: Great Battles
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Fighter
Spitfire Mk.XIV
History
Specifications

In 1934, Supermarine, a company known for producing record-breaking sports aircraft, presented the Type 224 monoplane at the Royal Air Force (RAF) competition for a new fighter. However, the project lost the competition, and the designers began to rework it: the resulting aircraft was radically different from the original. The Spitfire was a fast and maneuverable interceptor fighter. It had an original elliptical wing, a closed cockpit, and the latest Rolls-Royce PV12 engine (later called Merlin). The armament was increased from four to eight machine guns, with four in each wing. The prototype first flew on March 6, 1936, and the first production aircraft on May 15, 1938.

With the experience of the air war, the fighter was continuously improved. More and more advanced and powerful engines were installed and the armament was increased. By 1943 Rolls-Royce had developed the new powerful Griffin engine. The water-cooled engine, of the same V-shaped design as the Merlin, had slightly larger dimensions and weight but developed much more power. This engine with a two-stage compressor was installed in a new model of the Spitfire - Mk.XIV.

The Spitfire Mk.XIV is a single-seat, single-engine, all-metal monoplane with a cantilevered low wing. During production, the wing was also modified — additional fuel tanks were fitted in the leading edge. There were both standard and shortened wing tips. In late 1944, a cut-down rear fuselage and a teardrop-shaped cockpit canopy were introduced to improve visibility.

The first fighters were equipped with Griffon 61 engines, but they were quickly replaced by Griffon 65 engines, which developed a takeoff power of 2035 hp and up to 2450 hp in emergency mode using 150 octane fuel.

The armament of the first series of the Mk. XIV was installed in the Type C "Universal Wing." The armament configuration could vary, but in this series, the standard armament included two Hispano cannons (belt-fed) and four .303 Browning machine guns. In addition, racks for two 250 lb bombs could be mounted under the wings. The aircraft could carry a 500 lb bomb under the fuselage.

The first production aircraft entered combat service in January-February 1944. An important combat mission for the aircraft was to patrol the English coast in search of V-1 rockets after their launch. Seven Spitfire XIV squadrons were involved in the hunt for V-1s, the most successful of which was No. 91 Squadron, which destroyed 184.

The Spitfire XIV did not participate in the Normandy landings and did not arrive in France until the fall of 1944. They were mainly used as high-altitude fighters to maintain the air supremacy already established. With a speed advantage over all enemy aircraft except jets, Spitfire XIVs were able to attack any air target, even shooting down several jet fighters.

These aircraft were also used as fighter-bombers; at the front, the plane's armament was sometimes supplemented with rockets. Four FR XIV reconnaissance squadrons also operated in Europe. Some fighters and reconnaissance aircraft were transferred to India before the end of the war, but all three squadrons that received them had not reached combat readiness by the time Japan surrendered.

Used sources:
K. G. Munson "British Aircraft of World War II" 1962
V. Kotelnikov "Spitfire" The Best Fighter of the Royal Air Force" 2019
Materials from the site airwar.ru

Indicated stall speed in flight configuration: 152..172 km/h
Indicated stall speed in takeoff/landing configuration: 145..163 km/h
 
Dive speed limit: 756 km/h
Maximum load factor: 12.5 G
Stall angle of attack in flight configuration: 19.0 °
Stall angle of attack in landing configuration: 16.2 °
 
Maximum true air speed at sea level, 2750 RPM, boost +18: 574 km/h
Maximum true air speed at 4000 m, 2750 RPM, boost +18: 671 km/h
Maximum true air speed at 8100 m, 2750 RPM, boost +18: 720 km/h
 
Service ceiling: 13400 m
Climb rate at sea level: 23.8 m/s
Climb rate at 2650 m: 23.5 m/s
Climb rate at 6750 m: 18.2 m/s
 
Maximum performance turn at sea level: 18.1 s, at 270 km/h IAS.
Maximum performance turn at 3000 m: 21.0 s, at 260 km/h IAS.
 
Flight endurance at 3000 m: 1 h 45 m, at 350 km/h IAS.
 
Takeoff speed: 170..195 km/h
Glideslope speed: 180..210 km/h
Landing speed: 140..160 km/h
Landing angle: 12.5 °
 
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 2750 RPM and boost +18.
 
Engine:
Model: Griffon 65
Maximum power in Take-off mode (2750 RPM, boost +12, low gear) at sea level: 1565 HP
Maximum power in International power mode (2600 RPM, boost +9, low gear) at 4270 m: 1520 HP
Maximum power in International power mode (2600 RPM, boost +9, high gear) at 8070 m: 1375 HP
Maximum power in Emergency Max All Out mode (2750 RPM, boost +18, low gear) at 2134 m: 2063 HP
Maximum power in Emergency Max All Out mode (2750 RPM, boost +18, high gear) at 6400 m: 1845 HP
 
Engine modes:
Max Cruising power (unlimited time): 2400 RPM, boost +7
International power (up to 1 hour): 2600 RPM, boost +9
Emergency Max All Out power (up to 5 minutes): 2750 RPM, boost +18
 
Water rated temperature in engine output: 105..115 °C
Water maximum temperature in engine output: 135 °C
Oil rated temperature in engine intake: 90 °C
Oil maximum temperature in engine intake: 105 °C
 
Supercharger gear shift altitude: automatic with possibility of manual switch to low gear
 
Empty weight: 3295.0 kg
Minimum weight (no ammo, 10% fuel): 3422.7 kg
Standard weight: 3862.7 kg
Fuel load: 363.3 kg / 504.6 l / 111 gallons
Maximum useful load: 1027.8 kg
 
Forward-firing armament ("c-type" wing):
2 x 20mm gun "Hispano Mk.II", 150 rounds per gun, 650 rounds per minute, wing-mounted
4 x 7.7mm machine gun "Browning .303", 350 rounds per gun, 1150 rounds per minute, wing-mounted
 
Forward-firing armament ("e-type" wing):
2 x 20mm gun "Hispano Mk.II", 150 rounds per gun, 650 rounds per minute, wing-mounted
2 x 12.7mm machine gun "Browning .50", 250 rounds per gun, 850 rounds per minute, wing-mounted
 
Bombs:
2 x 250 lb general purpose bomb "250 lb. G.P."
500 lb general purpose bomb "500 lb. G.P."
 
Length: 9.9 m
Wingspan: 11.21 m
Wing surface: 22.48 m²
 
Combat debut: January 1944
 
Operation features:
- The engine is equipped with the automatic governor of the manifold pressure that works when the throttle is set to 1/3 position or above.
- The engine has a two stage mechanical supercharger which does not require manual control. It can be switched to the low gear manually.
- The engine is equipped with an automatic fuel mixture control which maintains optimal mixture.
- Engine RPM has an automatic governor that controls the propeller pitch to maintain the required RPM.
- The water and oil radiators shutters are operated automatically, but there is a special manual mode that forces radiator shutters to open completely.
- The aircraft has a neutral static stability. The elevator effectiveness is high, so the aircraft should be controlled carefully, not giving too much flight stick input.
- The aircraft becomes unstable with extended landing flaps.
- The aircraft is equipped with elevator and rudder trimmers.
- Landing flaps have a pneumatic actuator so they can be extended to maximum position only. Speed with extended landing flaps is limited to 160 mph.
- The aircraft tailwheel rotates freely and does not have a lock. Since the landing gear wheels are relatively close to each other, it is necessary to confidently and accurately operate the rudder pedals during the takeoff and landing.
- The aircraft has differential pneumatic wheel brakes with shared control lever. This means that if the brake lever is held and the rudder pedal the opposite wheel brake is gradually released causing the plane to swing to one side or the other.
- The aircraft is equipped with a siren that warns a pilot if the throttle is set to low position with landing gear retracted.
- It is impossible to open or close the canopy at high speed due to strong airflow. The canopy has an emergency release system for bailouts.
- The aircraft is equipped with two underwing formation lights.
- Standard gunsight is adjustable: both the target distance and target base can be set.
- The gyroscopic gunsight automaticly calculates required angular deflection while firing at a target. It has 4 modes: fixed reticle, fixed and gyro reticle, gyro reticle, gyro reticle with the target range fixed at 150 yards (night mode). The angular deflection will be calculated correctly only if the target range is set properly. To set the range, adjust the target base first using separate controls and then set the range by adjusting the size of the rangefiding reticle to be the same as the target size.
- Both gunsights have sliding sun-filters.
 
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 radiators control
- recommended position of the prop pitch control handle: light
- recommended position of the throttle lever: 5%
 
2. Recommended mixture control lever positions for various flight modes: auto mixture control
 
3. Recommended positions of the radiators control handle for various flight modes: auto radiators control
 
4. Approximate fuel consumption at 2000 m altitude:
- Cruise engine mode: 7.4 l/min
- Combat engine mode: 12.9 l/min
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