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Jan 14, 2023 at 2:05 comment added quiet flyer Are you planning to bet your life on an answer from ASE ; )
Jan 13, 2023 at 22:50 comment added sophit Yes perfect. Now you can put everything in the last diagram (the one with the "takeoff parameter" - use the second equation for propeller aircraft) of this answer and you should get a good approximation. Obviously you have to use takeoff values, with $C_{l_{TO}}$ being $1.21 \times C_{l_{max}}$. $\sigma$ is the density ratio in respect to ISA sea level.
Jan 13, 2023 at 20:31 comment added Justintimeforfun @sophit Does this help?
Jan 13, 2023 at 20:30 history edited Justintimeforfun CC BY-SA 4.0
edited body
Jan 13, 2023 at 20:19 history edited Justintimeforfun CC BY-SA 4.0
edited tags; edited title
Jan 13, 2023 at 19:22 comment added sophit You need the values of at least thrust, weight wing surface, density and maximum $C_l$, obviously all at takeoff. I think everything is know except max $C_l$ (?)
Jan 13, 2023 at 18:38 comment added HiddenWindshield @Justintimeforfun At least in the US, an ultralight must be less than 254 lbs. and carry 5 gallons or less of fuel. Since this plane has a gross weight of 850 lbs. and carries 26 gal. of fuel, it can't be an ultralight.
Jan 13, 2023 at 13:19 comment added GdD I'd call it fun!
Jan 13, 2023 at 2:10 comment added Justintimeforfun @quietflyer what would you call it?
Jan 13, 2023 at 0:17 comment added quiet flyer That is definitely not an ultralight!
Jan 12, 2023 at 21:50 history asked Justintimeforfun CC BY-SA 4.0