...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
