...its V-1710 and the aircraft's fuselage when need to accommodate the higher thrust and additional horsepower from the new engine. Curtiss removed all armament
29 KB (4,829 words) - 15:30, 16 January 2023
...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.
30 KB (4,925 words) - 21:44, 29 March 2024
...heat. Due to the position of the radiators, it gives a small amount of jet thrust to counteract the little drag it creates.
18 KB (2,945 words) - 18:50, 17 October 2023
...the more powerful Allison J33-A-35 engine that provided a 15% increase in thrust. Around 550 P-80Cs were fitted with the new engine. The P-80C also received
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
15 KB (2,316 words) - 18:30, 7 March 2024
...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%)
22 KB (3,479 words) - 22:46, 15 March 2024
...s early Allison engine proved to be weak on power when it came to take-off/thrust ratio and climbing speed. The distance needed to achieve the take-off roll
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
30 KB (4,835 words) - 20:55, 2 February 2024
...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%)
15 KB (2,360 words) - 15:19, 17 January 2023
...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%)
19 KB (3,093 words) - 11:27, 14 April 2024
...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%)
21 KB (3,355 words) - 10:15, 1 October 2023
...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%)
31 KB (4,974 words) - 11:52, 3 February 2024
...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
28 KB (4,705 words) - 00:49, 19 January 2024
...an the F2H-1. The Westinghouse J34-WE-34 engine provided an 8% increase in thrust and allowed for more pylons to be added to the airframe. This would also be
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
18 KB (2,907 words) - 11:16, 9 March 2024
...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 (WEP)
14 KB (1,996 words) - 09:57, 20 September 2023
...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%)
16 KB (2,583 words) - 16:50, 24 November 2023
...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%)
18 KB (2,817 words) - 14:10, 23 February 2024
...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%)
22 KB (3,439 words) - 19:43, 17 January 2024
...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%)
18 KB (2,813 words) - 22:48, 26 April 2024
* Strongest thrust/mass ratio of all Bf 109s in War Thunder
27 KB (4,268 words) - 02:41, 8 August 2023
...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.}}
17 KB (2,600 words) - 13:03, 5 December 2023
...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%)
21 KB (3,399 words) - 19:01, 7 April 2024
...ine, which only produced around 2,600 kgf. This provided an 8% increase in thrust and gave it substantially better performance in terms of acceleration, clim
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
15 KB (2,327 words) - 18:48, 13 October 2023
* Poor parasite drag to thrust ratio, meaning a lot of energy is lost in diving attacks due to wing surfac
21 KB (3,322 words) - 18:20, 12 February 2024
...was issued. The main upgrade was the new VK-1 engine, offering a lot more thrust. The East German air force would start receiving the upgraded MiG-15bis not
The MiG-15bis has a great thrust to weight ratio, allowing for amazing acceleration and energy retention. Pl
14 KB (2,146 words) - 05:42, 4 March 2024
...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%)
20 KB (3,125 words) - 20:57, 7 April 2024
...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%)
16 KB (2,566 words) - 22:26, 5 August 2022
...ing up the propeller pitch to high percentages will help bring out as much thrust from the engine as possible, which helps to compensate for the Yak-9P's wei
20 KB (3,107 words) - 09:48, 6 December 2022
...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%)
19 KB (2,961 words) - 19:53, 17 December 2023
...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%)
14 KB (2,234 words) - 22:44, 25 October 2023
...800-900 km/h), it's capable of more than 1,000 km/h at sea level when the thrust is set to 112%, note that this extra power consumes more fuel. However, the
...et fighters at similar battle rating, for example a F-84G, F2H or M.D.452. Thrust to weight ratio which is 0.45 is comparable to its main real life competito
16 KB (2,556 words) - 22:41, 25 October 2023
...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
26 KB (4,317 words) - 10:31, 4 November 2023
...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%)
23 KB (3,783 words) - 08:00, 25 October 2023
...up to 5,000 m in slightly above 2 minutes. The acceleration is also great, thrust to weight ration when the plane is fully loaded is 0.44, which is significa
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
21 KB (3,343 words) - 02:01, 16 December 2023
...arly form of afterburner/WEP, this new engine was supposed to increase the thrust of the MiG-9, but proved unreliable instead. The two aircraft with this eng
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
23 KB (3,785 words) - 11:53, 19 January 2024
The other noticeable change is a huge improvement of thrust-to-weight ratio which increased the acceleration by ~10% and it also has a
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
19 KB (2,906 words) - 13:03, 12 February 2024
...t to 6,000 m altitude in over two minutes. Since the MiG-17 is heavier its thrust to weight ratio is decreased and it affects its acceleration at low and med
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
19 KB (2,951 words) - 08:33, 24 October 2023
* Significant drop in thrust below 200 km/h, avoid stall climbs
16 KB (2,504 words) - 21:16, 26 February 2024
...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 (112%)
16 KB (2,586 words) - 08:19, 24 October 2023
...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
24 KB (3,931 words) - 15:41, 20 May 2023
...lays almost exactly the same: Relying on its very powerful engine and high thrust output to best its opponents in energy based engagements, while staying cau
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
13 KB (1,973 words) - 08:39, 24 October 2023
...its V-1710 and the aircraft's fuselage when need to accommodate the higher thrust and additional horsepower from the new engine. Curtiss removed all armament
24 KB (3,955 words) - 21:56, 21 October 2022
...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%)
14 KB (2,203 words) - 12:30, 16 March 2024
...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%)
13 KB (2,043 words) - 16:00, 18 February 2024
Its thrust to weight ratio is 0.50 with fuel tanks and 0.57 with 5 minutes of fuel, ma
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
17 KB (2,695 words) - 21:17, 23 December 2023
...eteor F Mk 4 G.41F may seem somewhat unappealing; it has the same mass and thrust, seemingly a very similar airframe, but a higher BR. However on closer insp
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
13 KB (1,993 words) - 13:46, 16 March 2024
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
! colspan="3" | Thrust to weight ratio @ 0 m (100%)
15 KB (2,333 words) - 13:45, 16 March 2024
...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%)
16 KB (2,499 words) - 13:45, 16 March 2024
...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%)
17 KB (2,637 words) - 13:12, 2 April 2024
...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%)
19 KB (2,964 words) - 20:08, 27 January 2024
...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
20 KB (3,188 words) - 01:06, 27 August 2022
...less stable than a normal tail plane thanks to a rear mounted engine push thrust configuration canard design, it is known for rapid pitch angle changes, gre
14 KB (2,281 words) - 13:23, 7 June 2023
