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  • ...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
  • ...unted on the RBT-5 tank have been updated: calibre, stabilizer parameters, thrust output and its deviation.
    24 KB (3,763 words) - 05:55, 13 July 2021
  • ...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
  • :* 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="4" | Thrust to weight ratio @ 0 m (100%)
    18 KB (2,816 words) - 14:41, 4 October 2023
  • :''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.
    170 KB (28,039 words) - 20:38, 14 May 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
  • ...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
  • ..."''' 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
  • ...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
  • ...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
  • ...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
  • ...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
  • ...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
  • ...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

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