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...output. Larger propellers were needed to transform more engine power into thrust, giving the Thunderbolt a boost in climb rate and acceleration. These prope ...ude climbing by converting more power from the enormous R-2800 engine into thrust.

...aircraft, the F4U-1A possesses the R-2800 radial engine, which has superb thrust and power at altitudes beginning at 3,000 metres and going up to around 6,5

...away; something in which the F6F is great at. They also provide increased thrust/lift and less speed when needed; for example during vertical slow speed dog

...at 150 km/h (92 mph/80 kt), flaps set to landing. Keep applying about 60% thrust, or as necessary to maintain 150 km/h. Touchdown at the beginning of the ca

* Strongest thrust/mass ratio of all Bf 109s in War Thunder

...ore its fuel supply falls low and it needs to land at an airbase. Its huge thrust-to-weight ratio guarantees however that the Komet will be able to engage th ...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}

* Poor parasite drag to thrust ratio, meaning a lot of energy is lost in diving attacks due to wing surfac

...peller-driven fighters. However, the engine only outputs around 910 kgf of thrust, which means it takes a very long time to accelerate up to suitable speeds. ...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}

...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}} ! colspan="5" | Thrust to weight ratio @ 0 m (100%)

...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}} ! colspan="5" | Thrust to weight ratio @ 0 m (100%)

...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}} ! colspan="5" | Thrust to weight ratio @ 0 m (100%)

...ombs. The I-153 entered Red Air Force service in October 1938 and was soon thrust into combat in the Far East, where the Soviet Union was engaged in an unoff

...angerous flutter of control stiffening regardless of whether you have full thrust or the engine is off. Here you will be more or less in your element, but th

...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}} ! colspan="5" | Thrust to weight ratio @ 0 m (109%)

...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}} ! colspan="6" | Thrust to weight ratio @ 0 m (100%)

...tly stick to Boom-and-Zoom tactics as the MB.5 has a high climb rate, high thrust power, and very high dive speed. * Contra-Rotating propeller, which provides amazing thrust

The Shusui's rocket engine provides quick acceleration and thrust and allows the plane to gain an altitude in relatively short time, even at ...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}

.... Though, if the {{PAGENAME}} gets behind one, the plane's slightly higher Thrust-to-Weigh ratio and flaps will help the {{PAGENAME}} stay behind it. (Still,

...away; something in which the F6F is great at. They also provide increased thrust/lift and less speed when needed; for example during vertical slow speed dog

...made, blades angle of attack decrease with increasing airspeed, so lesser thrust is produced. It means that the higher pitch is required. The higher the pit ...P-47_(Family)|P-47]] require micromanagement of mixture to provide maximum thrust. Most German and Italian fighters use a completely automated mixture contro

...pm and up to 650 kg thrust at sea level in take-off mode. Take-off booster thrust has been increased to 800 kg each. Their operating time has been reduced se

...ependence on thrust required for varying engine speeds has been corrected. Thrust for low engine speeds has been increased.

* Kikka - Thrust and high rudders has been added in the DM. * Po-2 - Thrust and high rudders have been fixed in the DM.

* Thrust will now be 0% on complete fuel exhaustion (when it is empty), the engine w ...te fuel tanks enabled. Fuel consumption rate depending on different engine thrust rating has been updated. Also refueling has been reworked - main tanks are

...mics and throttle engine performance has been corrected (dependency of the thrust from speed has been clarified). ...usly a missile reached its maximum speed at the maximum shot range. Engine thrust has been increased, thus a missile reaches a speed of 150 m/s within the fi

...unted on the RBT-5 tank have been updated: calibre, stabilizer parameters, thrust output and its deviation.

...R2 - engine-propeller combination has been re-worked (an error with higher thrust of the propeller on low speeds has been fixed). Engine RPM will now be more ...D5 - engine-propeller combination has been re-worked (an error with higher thrust of the propeller on low speeds has been fixed). Engine RPM will now be more

:* F-86 series engines thrust corrected to have more accurate optimal speed in a climb, according to refe

...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}} ! colspan="4" | Thrust to weight ratio @ 0 m (100%)

:''Hotline:'' how is the thrust-to-weight ratio of the [[F-15 (Family)|F-15]] calculated, what is the best ...longer it burns fuel, how effective is the [[Harrier (Family)|Harrier]]'s thrust vectoring during dogfights.

* The influence of the helicopters rotation on the tail rotor thrust has been clarified. The natural damping of single-rotor helicopters along t ...r flying the Wyvern S.4, where other single-engined aircraft would have no thrust or propeller rotation after spawning in them, has been fixed.

...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}} ! colspan="4" | Thrust to weight ratio @ 0 m (105%)

...xial flow on low speeds has been adjusted: climb rate goes to maximum when thrust is increasing. .... Controls have been improved, flight characteristics have been specified, thrust and control inversion chance has been decreased in excessive rotor pitch ac

..."''' missiles - corrected flight performance and seeker parameters: engine thrust has been increased, lateral acceleration has been decreased. * '''Gladiator Mk.II''' - bug has been fixed with thrust drop in WEP mode.

...s do well at [[Energy fighting]] due to a high rate of climb owed to their thrust to weight ratio.

...weight of engines in x-ray mode has been corrected; the max speed on 100% thrust has been increased.

...weight of engines in x-ray mode has been corrected; the max speed on 100% thrust has been increased.

...T-2]]''' — engine has been reworked (efficiency at high speeds with 100% thrust has been reduced slightly, climb rate in WEP mode has been slightly increas * '''[[BI]]''' — engine efficiency at low thrust has been corrected.

...been fixed with incorrect calculation of the parasitic drag for gun pods. Thrust reverse has been added.

...G-21, F-4 Phantom II, J-7 — excessive fuel consumption at low and medium thrust has been fixed.

...modelled on Mustangs. The cooling system is designed to generate a slight thrust that partially compensates for the aerodynamic drag caused by the radiators

* '''AJ37, JA37C''' — a bug has been fixed that caused a reverse thrust malfunction ([https://community.gaijin.net/issues/p/warthunder/i/MFDspjc0uM

* Jaguar GR.1, Jaguar A — Insufficient engine thrust has been fixed. ...ved. Influence of engine thrust on aircraft balancing (instability on full thrust will be insignificantly increased) has been implemented.

* '''Yak-38,Yak-38M''' 一 incorrect indication of the thrust direction in the cockpit has been fixed .

...been adjusted 40 sec → 23 sec, max overload 20 G → 30 G, instantaneous thrust 36 kN → 27.9 kN. ...- a bug has been fixed that caused an incorrect engine speed and available thrust.

* '''Mirage F1C''' — available thrust at medium (M 0.4…0.7) speeds at low and medium altitudes has been adjuste ...aps animation has been fixed, animation of the intake hatches when reverse thrust is engaged has been fixed.

...odifications)''' — The effect of rebalancing the aircraft at full engine thrust has been refined (on full control, you can see a slight nose down pull). Th * '''Mirage F1C (all versions)''' — Engine thrust at supersonic speeds has been increased. Climbrate at sea level and at alti

...accelerate to its top speed, and then it will enter a state of continuous thrust. Missile guidance improves with speed, however it will have a tendency to p

* Aircraft controls (control stick, thrust lever and rudder pedals) now emit sounds when moved inside the cockpit view