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There is a page named "Talk:Thrust-to-weight ratio" on Wikipedia
- to be more than 0.1654" Thrust to WEIGHT ratio always need to be larger than unity. Moon's surface gravity 1/6 of Earth, but you still need 1N thrust...13 KB (1,944 words) - 13:56, 14 June 2024
- Since we have the power/weight ratio of batteries and fuel cells, it would be interesting to compare this with petrol and diesel fuels, too. Also could...38 KB (5,653 words) - 14:04, 23 March 2024
- be used on a stage, but the thrust values in the table are for a single engine. For the thrust to weight ratio, the weight is mass times earth's acceleration...26 KB (3,929 words) - 04:55, 29 January 2024
- comes in because the wing has a L/D ratio, and which gives the ratio of weight to thrust. The amount of fuel needed to carry it comes from the SFC. So a...18 KB (2,659 words) - 05:50, 7 February 2024
- other vehicle component weights." Seems pretty clearcut. To be honest you rarely or never see *any* aerospace thrust/weight ratio specified in lbf/lb or...16 KB (2,441 words) - 20:46, 24 February 2024
- Talk:NK-33 (section Thrust/weight)weight to the engine, thus reducing the thrust-to-weight ratio. If the NK-33 included the gimballing, and thrust support, it's thrust-to-weight ratio...23 KB (3,671 words) - 18:17, 21 February 2024
- Talk:General Electric CF6 (section Thrust/weight)metric, since they are American designs. The Thrust-to-weight ratio for these engines would be nice to have, if someone has the information. See http://en...3 KB (365 words) - 14:48, 1 February 2024
- rocket engines: RD-270 - thrust-to-weight ratio was 201:1 RD-253 - thrust-to-weight ratio was 172:1 RD-701 - thrust-to-weight ratio was 212:1 Shpankov (talk)...79 KB (11,607 words) - 18:06, 26 March 2024
- Talk:Ryan X-13 Vertijet (category Military history articles needing attention to referencing and citation)had a thrust-to-weight ratio of 1 at low fuel quantities,..." but in the data it lists 1.48. Is this correct? Bubba73 You talkin' to me? 19:51, 11 August...3 KB (261 words) - 23:49, 8 February 2024
- Talk:Gaseous fission reactor (section Thrust-to-weight)be heated enough to use the full efficiency of the fuel, while still getting high specific impulse? The highest thrust-to-weight ratio I ever heard of...2 KB (351 words) - 10:58, 21 May 2024
- supposedly maximum thrust/weight according to the edit, is smaller than the ratio 1.213, supposedly normal thrust to weight according to the edit. Applying...45 KB (6,911 words) - 01:57, 18 October 2023
- Talk:Guizhou JL-9 (category Aviation articles needing attention to referencing and citation)needs to redo the math on that thrust to weight ratio, 1.31 is just stupid, the loaded weight exceeds maximum AB thrust, and the empty weight exceeds...2 KB (162 words) - 00:50, 29 February 2024
- Talk:Boeing F-15EX Eagle II (category Military history articles needing attention to coverage and accuracy)and the F-15EX is slightly more than that. Thrust-to-weight ratio here is typically for loaded gross weight, although much of the numbers here are just...14 KB (2,089 words) - 17:59, 2 March 2024
- reduction in orbital weight by airbreathing is small, whereas airbreathing engines have a poor thrust/weight ratio which tends to increase the orbital...33 KB (4,886 words) - 12:19, 10 March 2024
- Talk:Beriev Be-2500 (category Aviation articles needing attention to coverage and accuracy)Secondly, how is the thrust/weight ratio calculated? Is it reasonable (in the particular case) to base it on sea level thrust (sensible for an ekranoplan)...10 KB (1,392 words) - 05:50, 28 January 2024
- Talk:Volvo RM12 (category Aviation articles needing attention to grammar)The article shows a t/w ratio of 7.8 thrust to 1 weight. Is this dry-thrust or wet-thrust? — Preceding unsigned comment added by 2001:984:9921:1:5945:3585:3C68:719C...738 bytes (41 words) - 18:43, 28 January 2024
- showing lift, weight, thrust and drag is not entirely correct. In UNACCELERATED flight all OPPOSING forces are equal. The diagram shows thrust being greater...32 KB (5,125 words) - 15:36, 15 February 2024
- in order to add it. -Nem1yan (talk) 14:54, 25 April 2011 (UTC) Why is the thrust to weight ratio for the J-11A so low ? Only 0,66 dry thrust even the...21 KB (2,797 words) - 13:30, 19 July 2024
- lbs thrust each (dry thrust), thrust to weight = 0.448, rate of climb 6,200 fpm. T-38 supersonic jet trainer: Max take off weight 12,093 lbs, 2X J85 engines...7 KB (1,137 words) - 14:10, 31 January 2024
- How atoms/particles change the ratio? is it possible? - Unsigned Please see WP:RD to get an answer to you question =) --mboverload@ 00:22, 14 May 2006...32 KB (4,704 words) - 13:20, 7 February 2024
- Reliable data from the developing world on the ratio of abortions to pregnancies are limited almost entirely to those Asian countries in which abortion is
- gravity, in direct ratio to the displacement of this new force, forward, backward, to right or left of the perpendicular. If the man's weight shifts forward
- Gas-turbine engines are widely used to power aircrafts because of their light-weight, compactness, and high power-to-weight ratio. Aircraft gas turbines operate