...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
