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  • ...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
  • ...abrik factory. The {{Specs|name}} was the only surviving example of the Ho 229, and it is currently on display at the Smithsonian National Air and Space M ...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
    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="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 (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="3" | Thrust to weight ratio @ 0 m (100%)
    12 KB (1,800 words) - 13:47, 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%)
    16 KB (2,524 words) - 16:17, 18 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%)
    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
  • ...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
  • ...X-Wing has become the mainstay of the rebel alliance although the [[Ho 229 V3|Y-Wing]] still holds the record for the most [[Me 262 A-1a|TIE Fighters]] d Unlike the [[Ho 229 V3|Y-Wing]], the X-Wing has a very sleek shape. The whole fighter is needle sh
    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)
    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="5" | Thrust to weight ratio @ 0 m (100%)
    20 KB (3,171 words) - 16:16, 4 January 2024
  • ...peed of any supersonic jet (78 knots, 145 km/h, equivalent to the [[Ho 229 V3]] and [[Bf 109 E-4|Bf 109 E]]), it has slightly more than twice the availab ...ximum thrust produced by each engine, while mounted in the aircraft. NOTE: Thrust varies significantly depending on speed & altitude.}}
    31 KB (4,782 words) - 13:02, 16 March 2024