It may seem very simple but I want to be absolutely certain of this :
Can I say that a model rocket with a mass of 1 kilogram and a thrust of 1 kilogram-force has a Thrust/Weight ratio of 1:1 ?
(at liftoff (T+0), practically the mass will lower as the fuel is burned).
Can I say that a model rocket with a mass of 1 kilogram and a thrust of 1 kilogram-force has a Thrust/Weight ratio of 1:1 ?
(at liftoff (T+0), practically the mass will lower as the fuel is burned).