...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
...excess of 1,100 km/h (683 mph). However, the J47 engine has relatively low thrust output, and it takes time to reach significant speeds. One of the main adva
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
15 KB (2,356 words) - 10:04, 19 November 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%)
20 KB (3,184 words) - 20:51, 23 March 2024
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.}}
22 KB (3,432 words) - 19:22, 2 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%)
14 KB (2,288 words) - 21:08, 1 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%)
15 KB (2,439 words) - 21:08, 1 April 2024
.... 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,
22 KB (3,568 words) - 17:49, 11 April 2023
...of thrust this first look disadvantage is literally outweighed by the high thrust to weight ratio of 0.73 empty (0.41 full). This makes the Gina an excellent
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
16 KB (2,570 words) - 14:13, 4 January 2024
...of thrust this first look disadvantage is literally outweighed by the high thrust to weight ratio of 0.73 empty (0.41 full). This makes the Gina an excellent
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
19 KB (2,969 words) - 14:11, 4 January 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%)
31 KB (5,012 words) - 12:22, 3 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%)
13 KB (2,029 words) - 01:01, 4 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%)
29 KB (4,643 words) - 12:20, 3 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 (110%)
13 KB (1,997 words) - 18:41, 23 December 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%)
21 KB (3,277 words) - 20:51, 23 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%)
22 KB (3,435 words) - 10:21, 23 December 2023
...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
17 KB (2,773 words) - 20:35, 11 December 2022
* thrust_mult: Multiplies the unit's thrust by the given amount. This does not allow the unit to bypass its speed limit
169 KB (25,588 words) - 13:40, 11 April 2024
...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
62 KB (9,172 words) - 16:28, 1 June 2019
...ependence on thrust required for varying engine speeds has been corrected. Thrust for low engine speeds has been increased.
70 KB (10,724 words) - 09:12, 27 December 2023
* Kikka - Thrust and high rudders has been added in the DM.
* Po-2 - Thrust and high rudders have been fixed in the DM.
49 KB (7,634 words) - 22:38, 7 May 2024
* 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
42 KB (6,568 words) - 05:56, 13 July 2021
...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
31 KB (4,757 words) - 14:37, 6 December 2023
...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
20 KB (3,175 words) - 21:03, 5 January 2019
If using Manual Engine Controls, turn up the propeller pitch for maximum thrust and open the radiators by a tiny amount, no more than single digit percenta
25 KB (4,126 words) - 05:31, 18 December 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 (WEP)
17 KB (2,377 words) - 12:50, 4 May 2024
:* F-86 series engines thrust corrected to have more accurate optimal speed in a climb, according to refe
20 KB (3,072 words) - 18:41, 12 September 2021
...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 (WEP)
32 KB (5,167 words) - 11:32, 16 August 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%)
14 KB (2,040 words) - 20:50, 23 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 (WEP)
18 KB (2,875 words) - 11:57, 24 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%)
18 KB (2,816 words) - 14:41, 4 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 (WEP)
21 KB (3,321 words) - 08:28, 29 September 2023
...4 liquid propellant motor to produce a range of up to 11 km and produced a thrust of 12,000 pounds or 53 kN. The production of AGM-12B ended in 1970 and 22,0
7 KB (1,113 words) - 10:16, 13 November 2023
...et was not much heavier than the J47, while it produced significantly more thrust. The version that used the J65 turbojet engine was designated as the FJ-3 F
9 KB (1,420 words) - 21:40, 24 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%)
16 KB (2,561 words) - 12:37, 18 January 2024
|'''Thrust'''
12 KB (1,937 words) - 11:37, 24 August 2022
:''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.
168 KB (27,749 words) - 18:00, 21 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 (WEP)
16 KB (2,422 words) - 14:15, 4 January 2024
...erplant is the Rolls-Royce Nene Mk.103 engine, which gives it quite decent thrust to weight ratio of 0.40 with full fuel tanks. The plane is not that fast, a
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
17 KB (2,618 words) - 12:43, 18 January 2024
...he Mk 6 was powered by the Orenda 14 engine. It provided a 14% increase in thrust and greatly improved the Mk 6's performance. The climb rate, top speed, and
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
18 KB (2,775 words) - 23:31, 13 October 2023
...the MiG-19S is able to accelerate very well at all speeds and can use this thrust to achieve a considerable climb rate matched by nearly no other aircraft at
...with a touchdown at over 350 km/h being easily possible. The plane's high thrust-to-weight also allows it to take off quicker than most other jets it will f
19 KB (2,886 words) - 09:16, 26 April 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 (WEP)
32 KB (4,997 words) - 21:41, 7 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 (WEP)
19 KB (2,882 words) - 08:25, 25 October 2023
...f thrust, this first look disadvantage is literally outweighed by the high thrust to weight ratio of 0.73 empty (0.41 full). This makes the Gina an excellent
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
23 KB (3,609 words) - 13:14, 25 June 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%)
14 KB (2,132 words) - 12:51, 6 February 2024
* 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.
62 KB (9,227 words) - 09:24, 12 September 2019
...xtremely manoeuvrable but also extremely short range SRAAM missiles, whose thrust-vectoring capabilities allow them to easily hit targets at most angles with
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
27 KB (4,259 words) - 04:57, 11 April 2024
...r driveshaft besides the engines is the most important part of maintaining thrust, as if it is damaged too much the engine condition will not matter and a lo
20 KB (3,120 words) - 05:07, 21 January 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 (WEP)
16 KB (2,441 words) - 21:28, 23 December 2023
...ghly manoeuvrable infrared homing air-to-air missile. The missile's use of thrust vectoring, and an IR seeker with very wide gimbal limits, means that it can
Thrust vectoring also allows the missiles to start manoeuvring immediately after l
16 KB (2,728 words) - 08:23, 1 January 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 (105%)
22 KB (3,495 words) - 12:45, 22 January 2024
...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
62 KB (9,538 words) - 10:00, 27 June 2020
...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 (2,900 words) - 08:27, 9 October 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%)
17 KB (2,780 words) - 07:53, 2 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 (108%)
16 KB (2,686 words) - 11:55, 19 January 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%)
14 KB (2,130 words) - 16:30, 24 December 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%)
24 KB (3,800 words) - 12:19, 3 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 (WEP)
20 KB (3,189 words) - 12:38, 21 September 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%)
13 KB (1,957 words) - 12:38, 21 September 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 (WEP)
18 KB (2,832 words) - 21:29, 5 September 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 (WEP)
24 KB (3,818 words) - 13:42, 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 (WEP)
54 KB (8,883 words) - 17:51, 16 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 (WEP)
15 KB (2,329 words) - 21:32, 23 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 (WEP)
22 KB (3,659 words) - 09:27, 24 December 2023
...or over-revving the propeller. Using the collective at 100% will increase thrust (useful when altitude is needed) but will reduce the horizontal speed drast
19 KB (3,077 words) - 15:21, 29 November 2023
...i-armour piercing and weighed 450 kg. The motor generated 33,000 pounds of thrust or 147 Kn, to produce a range of 16 km. The total amount produced was aroun
4 KB (535 words) - 21:32, 13 December 2022
...from a Rolls-Royce Avon Mk. 113 engine with 3,188 kgf, however, the final thrust output was no contest with the {{PAGENAME}} able to fly 1,000 km/h faster t
! Zero-Thrust, 1G Stall speed<br>(km/h)
29 KB (4,640 words) - 13:36, 16 March 2024
...werplant is the Bristol Orpheus MK.803 engine that can produce 2270 kgf of thrust. The level speed is quite good: it can reach 1,084 km/h at sea level, sligh
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
19 KB (2,957 words) - 14:24, 28 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%)
24 KB (3,823 words) - 10:57, 21 April 2024
...FB.52A variants in particular had a new Goblin 3 engine that offered more thrust than the FB.5's Goblin 2. After the delivery of the 51 Vampire FB.52As, Ita
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
14 KB (2,201 words) - 12:32, 16 March 2024
...who has flown the F-86A-5. The engine feels lacking; it does produce more thrust than the contemporary [[MiG-15]]'s RD-45 engine, but considering that the S
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
18 KB (2,784 words) - 04:52, 16 October 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 (WEP)
14 KB (2,136 words) - 06:40, 2 June 2022
...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 (2,692 words) - 22:10, 28 September 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 (WEP)
29 KB (4,706 words) - 21:34, 25 September 2023
..."''' 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.
67 KB (10,307 words) - 09:00, 6 June 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 (WEP)
28 KB (4,573 words) - 23:02, 12 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 (WEP)
20 KB (3,234 words) - 10:07, 28 January 2024
...ojet engines found on American Phantoms. The British engines produced more thrust than the American engines, but were larger; as a result, the fuselage of Br
...one of the most powerful jet engines in the game and give it an incredible thrust to weight ratio, leading to the Phantom FGR.2 being the fastest acceleratin
38 KB (6,007 words) - 06:24, 14 April 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%)
23 KB (3,569 words) - 20:11, 9 March 2024
...0.5 seconds less than the AIM-9D, while also producing less than half the thrust, which coupled with its lower top speed and much lower flight time and flig
15 KB (2,481 words) - 18:13, 25 March 2023
* The aerodynamics, motor thrust, and firing duration of the missile.
42 KB (6,770 words) - 16:43, 31 March 2024
This statment holds at a constant engine thrust <big>'''F'''</big> affecting to the mass of the airplane <big>'''m'''</big>
8 KB (1,429 words) - 10:54, 27 July 2023
...targets. Developed from the FFAR "Mighty Mouse", a new motor produces more thrust and increases the effective range of the Hydra, and a new fin design improv
6 KB (967 words) - 18:34, 3 April 2024
...s do well at [[Energy fighting]] due to a high rate of climb owed to their thrust to weight ratio.
13 KB (2,183 words) - 11:59, 7 November 2019
...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%)
18 KB (2,814 words) - 19:53, 7 April 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%)
18 KB (2,757 words) - 20:10, 22 November 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%)
19 KB (3,150 words) - 20:18, 22 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%)
19 KB (3,001 words) - 00:55, 11 October 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 (WEP)
24 KB (3,952 words) - 21:28, 4 May 2024
...g enemies far beyond the plane's reach. This, combined with the incredible thrust, lets the '''{{PAGENAME}}''' decide when, and how to strike down opponents;
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
24 KB (3,762 words) - 16:52, 12 April 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%)
20 KB (3,171 words) - 16:16, 4 January 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 (WEP)
19 KB (2,942 words) - 13:24, 16 March 2024
...top speed. One more notable feature is that due to its low weight and high thrust, energy management is a breeze and the aircraft will quickly both lose and
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
22 KB (3,506 words) - 13:27, 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%)
17 KB (2,563 words) - 10:04, 28 January 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 (WEP)
19 KB (2,851 words) - 04:21, 26 March 2024
...plant is the Pratt & Whitney J57-P-16 engine that can produce 8,000 kgf of thrust. The Crusader is able to reach 1 Mach in level flight at sea level and 1.95
...ot that easy, so the player does not have to worry about overspeeding. Its thrust to weight ratio while not being close to 1.0 still is good enough to make t
39 KB (6,393 words) - 06:40, 9 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 (WEP)
32 KB (5,026 words) - 15:17, 6 May 2024
...J65-W-16A engine that can produce up to 3,200 kgf of thrust giving it good thrust to weight ratio. At sea level it can reach up to 1063 km/h, that puts it on
...interceptors, for example the MiG-15. The plane accelerates very well, the thrust to weight ratio is 0.47 with full fuel tanks and can be increased to 0.59 a
26 KB (4,077 words) - 13:12, 26 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 (WEP)
38 KB (5,978 words) - 04:31, 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 (WEP)
20 KB (3,008 words) - 00:22, 5 November 2023
...points, and no flaps. It also has an early J57P7 engine that produces less thrust than the D model's J57P21. The speed and acceleration remained comparable s
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
20 KB (3,288 words) - 17:37, 7 December 2023
...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 (WEP)
31 KB (4,782 words) - 13:02, 16 March 2024
...n-First-Line|}}World's Leading Distributor of MiG Parts{{-}}The triumph of thrust over aerodynamics
4 KB (503 words) - 15:43, 21 September 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%)
11 KB (1,587 words) - 11:51, 3 February 2024
...weight of engines in x-ray mode has been corrected; the max speed on 100% thrust has been increased.
99 KB (14,925 words) - 09:00, 6 June 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 (WEP)
21 KB (3,419 words) - 05:00, 13 November 2023
...tion was rejected. The F-104C also features a better engine that increased thrust by about 7% thanks to the 3-inch increase in the turbine's diameter. Minor
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
25 KB (4,008 words) - 12:24, 3 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 (WEP)
25 KB (3,905 words) - 04:01, 17 January 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 (WEP)
16 KB (2,415 words) - 18:41, 7 April 2024
...odynamics and powerful engine, the General Electric J79-GE-11; which gives thrust of up to 4,130 kgf without and 8,391 kgf with afterburner. This is achieved
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
25 KB (3,915 words) - 04:51, 20 December 2023
...f thrust, this first look disadvantage is literally outweighed by the high thrust to weight ratio of 0.73 empty (0.41 full). This makes the Gina an excellent
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
17 KB (2,595 words) - 15:59, 30 January 2024
...ised by a low BR for a supersonic jet and amazing acceleration. With a 1-1 thrust-weight ratio when at optimal fuel load and spaded, it can reliably punch ab
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
21 KB (3,282 words) - 17:22, 24 September 2023
...d in part by a special flap-blowing system that allowed some of the excess thrust to be redirected across the flaps to reduce its stall speed, over half of t
...ines. The Scimitar's two Rolls-Royce Avon 202 engines put out 4,650 kgf of thrust each, giving the Scimitar its fantastic climb rate of over 100 m/s. This ou
24 KB (3,735 words) - 23:08, 12 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 (WEP)
35 KB (5,525 words) - 20:06, 17 June 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 (WEP)
21 KB (3,304 words) - 20:51, 31 December 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%)
27 KB (4,375 words) - 20:50, 23 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 (WEP)
19 KB (2,936 words) - 13:34, 7 September 2023
The F-104G has about 8% more engine thrust than the F-104A in exchange for slightly increased weight. The general perf
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
21 KB (3,290 words) - 04:49, 20 December 2023
...ne has the highest thrust of all F-104 variants by a large margin: optimal thrust on afterburner is about 22% greater than the J79-GE-11 used by the [[F-104G
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
25 KB (3,879 words) - 14:15, 23 February 2024
...b handling characteristics in a deep stall, allowing rapid-reaction vector-thrust-like manoeuvrability albeit the yaw control being commanded by the inverse
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
26 KB (3,988 words) - 18:33, 12 April 2024
...c 1 missile. Note the size and number of control surfaces, and the lack of thrust vectoring in the missile's rocket motor nozzle.</small>
7 KB (1,134 words) - 16:46, 10 January 2024
* '''[[F4U-1C]]/[[F4U-1D|D]]''' — an engine bug causing insufficient thrust has been fixed.
45 KB (6,889 words) - 17:13, 16 June 2022
...weight of engines in x-ray mode has been corrected; the max speed on 100% thrust has been increased.
70 KB (10,540 words) - 17:16, 16 July 2020
...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 (WEP)
16 KB (2,408 words) - 12:06, 7 May 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)
31 KB (5,295 words) - 15:01, 9 December 2023
...s modeled on Mustangs. The cooling system is designed to generate a slight thrust that partially compensates for the aerodynamic drag caused by the radiators
19 KB (3,057 words) - 12:41, 22 January 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 (WEP)
23 KB (3,567 words) - 13:02, 6 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 (WEP)
19 KB (2,860 words) - 18:43, 21 October 2023
...area, yet it boasts two jet engines, each yielding nearly two tons of wet thrust. These characteristics give the Jaguar high agility and responsiveness, bei
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
20 KB (3,074 words) - 21:33, 25 October 2023
...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%)
18 KB (2,714 words) - 16:22, 23 January 2024
...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.
43 KB (6,637 words) - 10:40, 16 December 2020
...[[Harrier (Family)|Harrier family]], the AV-8C is a [[VTOL]] aircraft with thrust vectoring nozzles, which allow it to take off and land vertically. In terms
| 1,687 kg || colspan="2" | Vectored-thrust low-bypass turbofan
18 KB (2,756 words) - 20:37, 31 January 2024
...ly)|Harrier family]], is capable of vertical take-off and landing with its thrust vectoring nozzles, in addition to enhancing its manoeuvrability. Among the
| 1,687 kg || colspan="2" | Vectored-thrust low-bypass turbofan
20 KB (2,980 words) - 13:36, 9 November 2023
| 1,420 kg (main) || colspan="2" | Vectored-thrust axial-flow turbojet
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
21 KB (3,160 words) - 21:51, 3 November 2023
...nd on short runways, roads, or even ships, using a combination of vectored thrust and reaction control systems. This gave it a tactical advantage over conven
...(Family)|Harrier family]], the {{Specs|name}} is a [[VTOL]] aircraft with thrust vectoring nozzles, which allow it to take off and land vertically. This ver
34 KB (5,308 words) - 08:21, 24 October 2023
...A.1 prototype aircraft that demonstrated the feasibility of using vectored thrust to achieve V/STOL capability. Recognizing the potential of this technology
...er (Family)|Harrier family]], the Harrier GR.1 is a [[VTOL]] aircraft with thrust vectoring nozzles, which allow it to take off and land vertically. The Harr
31 KB (4,943 words) - 20:06, 13 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 (WEP)
21 KB (3,207 words) - 18:37, 26 April 2024
...more than compensated by the fact that its engines produce about 15% more thrust. Its top speed is now practically the same as or in some cases slightly bet
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
24 KB (3,746 words) - 10:01, 19 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 (102%)
32 KB (4,990 words) - 13:45, 30 March 2024
...was being developed around the new Tumansky R-25 engine, which promised a thrust-to-weight ratio of over 1 on full second-stage afterburner when mated to a
...he new addition of the new R-25-300 engine, giving this aircraft increased thrust over its older variants. The other major upgrade to the MiG-21bis is its fi
20 KB (3,173 words) - 18:38, 26 April 2024
...hawk family. It had the J52-P-6A engine which produced almost 3,500 kgf of thrust. Most importantly, the P-6A had far better fuel efficiency which increased
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
25 KB (3,914 words) - 12:16, 7 May 2024
...force will be additionally increased with full flap deflection and 30-50% thrust to provide lower landing speeds.
...parameters in the BOLIDE missile for ASRAD-R have been fixed. Rocket motor thrust has been increased. The warhead is now a shaped charge/fragmentation, simil
40 KB (6,061 words) - 09:00, 6 June 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%)
25 KB (3,921 words) - 13:15, 26 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%)
16 KB (2,285 words) - 10:04, 23 September 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%)
17 KB (2,663 words) - 21:29, 28 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%)
15 KB (2,241 words) - 11:31, 9 July 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%)
37 KB (6,022 words) - 17:23, 13 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%)
15 KB (2,243 words) - 13:25, 22 January 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%)
16 KB (2,328 words) - 10:09, 28 January 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 (WEP)
25 KB (3,904 words) - 13:39, 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 (WEP)
13 KB (1,973 words) - 13:28, 31 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 (WEP)
17 KB (2,663 words) - 17:01, 1 January 2024
...been fixed with incorrect calculation of the parasitic drag for gun pods. Thrust reverse has been added.
76 KB (12,084 words) - 21:30, 10 September 2021
...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%)
12 KB (1,731 words) - 21:57, 23 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 (WEP)
27 KB (4,346 words) - 03:54, 24 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 (WEP)
26 KB (4,137 words) - 14:29, 25 July 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 (WEP, no booster)
21 KB (3,233 words) - 12:44, 21 January 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 (WEP)
16 KB (2,472 words) - 14:06, 30 October 2023
...f flaps !! Landing flaps !! Air brakes !! Arrestor gear !! Drogue chute !! Thrust reversal
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
19 KB (2,865 words) - 15:17, 7 March 2024
...G-21, F-4 Phantom II, J-7 — excessive fuel consumption at low and medium thrust has been fixed.
120 KB (18,640 words) - 09:00, 6 June 2023
...modelled on Mustangs. The cooling system is designed to generate a slight thrust that partially compensates for the aerodynamic drag caused by the radiators
21 KB (3,443 words) - 09:49, 17 May 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 (3,060 words) - 04:42, 14 August 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%)
16 KB (2,524 words) - 03:41, 20 January 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 (WEP)
18 KB (2,808 words) - 11:30, 21 April 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 (WEP)
26 KB (4,154 words) - 15:30, 8 April 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 (WEP)
25 KB (3,862 words) - 12:56, 14 November 2023
...es (licensed copies of the [[F-4E]]'s engines), each providing 8010 kgf of thrust when spaded, F-4F provides solid performance at any altitude.
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
26 KB (4,101 words) - 14:57, 11 April 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 (WEP)
20 KB (3,044 words) - 18:41, 26 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%)
23 KB (3,564 words) - 11:14, 3 February 2024
...s behind the [[MiG-21SMT]] and [[MiG-21bis]]'s engines in terms of maximum thrust, the J-7E actually weighs less than the [[MiG-21MF (Germany)|MiG-21MF]] and
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
29 KB (4,858 words) - 08:56, 14 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 (WEP)
22 KB (3,487 words) - 17:07, 9 March 2024
* '''AJ37, JA37C''' — a bug has been fixed that caused a reverse thrust malfunction ([https://community.gaijin.net/issues/p/warthunder/i/MFDspjc0uM
58 KB (9,220 words) - 09:00, 6 June 2023
...ort tail. Meanwhile, the J35A2 (long) had a new afterburner with increased thrust, which meant that the tail section needed to be extended. While unexpectedl
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
15 KB (2,274 words) - 21:37, 4 May 2024
...t. The F-8E is particularly strong at lower speeds, where the extra engine thrust allows it to sustain turns and accelerate quicker, and it also inherits the
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
26 KB (4,143 words) - 00:25, 1 February 2024
...jet version, the MiG-23M, the MiG-27M is slightly heavier and has a lower thrust (despite the difference being very little). As a result, the MiG-27M can pu
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
21 KB (3,305 words) - 03:45, 24 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 (WEP)
16 KB (2,258 words) - 12:23, 29 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 (WEP)
27 KB (4,267 words) - 03:54, 8 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 (WEP)
15 KB (2,319 words) - 18:54, 24 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 (WEP)
18 KB (2,873 words) - 18:35, 8 January 2024
...omputer. The GR.1A also featured Adour Mk. 104 engines, offering increased thrust and performance over the original GR.1 model’s engines. This resulted in
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
26 KB (4,064 words) - 18:37, 21 October 2023
* 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.
48 KB (7,571 words) - 04:40, 19 July 2022
..."pointing" the nose at the enemy aircraft in most situations, and the raw thrust the MiG has will also allow for a degree of stallfighting. However, as a de
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
20 KB (3,145 words) - 18:39, 26 April 2024
...flight performance upgrades, the powerful R-35F-300 engine providing extra thrust over older MiG-23 models was installed. The radar was replaced with the bra
...ed on the MLD because its engine is 20% more powerful, and as a result its thrust-to-weight ratio practically matches the [[F-104S]] and [[MiG-21bis]]. It ha
28 KB (4,455 words) - 03:45, 24 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%)
18 KB (2,719 words) - 22:06, 6 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 (WEP)
20 KB (2,987 words) - 05:25, 18 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 (WEP)
57 KB (9,588 words) - 07:31, 6 April 2024
* '''Yak-38,Yak-38M''' 一 incorrect indication of the thrust direction in the cockpit has been fixed .
65 KB (9,824 words) - 09:00, 6 June 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%)
12 KB (1,810 words) - 14:39, 13 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%)
12 KB (1,854 words) - 13:00, 28 April 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 (WEP)
17 KB (2,658 words) - 21:16, 5 September 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 (WEP)
15 KB (2,381 words) - 21:15, 4 May 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%)
12 KB (1,753 words) - 02:40, 5 October 2023
...y light airframe and powerful J52-P-8A engine which provides a respectable thrust-to-weight ratio. The two 30 mm cannons are devastating to enemy aircraft as
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
14 KB (2,203 words) - 22:07, 6 November 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 (WEP)
45 KB (7,258 words) - 04:37, 29 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 (WEP)
19 KB (2,742 words) - 14:17, 23 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 (WEP)
23 KB (3,577 words) - 13:08, 14 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 (WEP)
20 KB (3,066 words) - 17:46, 6 April 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 (WEP)
24 KB (3,709 words) - 05:26, 28 April 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 (WEP)
18 KB (2,907 words) - 10:52, 21 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 (110%)
15 KB (2,305 words) - 17:49, 6 April 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%)
15 KB (2,359 words) - 12:29, 28 April 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%)
15 KB (2,215 words) - 12:26, 23 September 2023
