...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
...eor once this immediate issue has been mitigated, and has more than enough thrust to regain speed or separation after an engagement.
...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
15 KB (2,354 words) - 21:54, 27 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 (109%)
18 KB (2,754 words) - 21:09, 27 May 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 (2,360 words) - 17:40, 19 May 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%)
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
