Weight and rate of climb are directly related when engine power remains constant.
One Ex to another: t'aint that simple, lad. pbehn's pesky variables all add into the equation. Two engines of the same horsepower don't necessarily produce the same thrust unless they have identical props and superchargers rigged identically. Different marks of the same airframe almost certainly will not have identical drag coefficients due to different armament, antenna, and various other details. I could go on and on, but it's like conversing with a brick wall.It isnt a question of just weight, it is thrust lift drag etc.