High Quality Content by WIKIPEDIA articles! The Tsiolkovsky rocket equation, or ideal rocket equation, is a mathematical equation that relates the delta-v with the effective exhaust velocity and the initial and final mass of a rocket. The equation is named after Konstantin Tsiolkovsky who independently derived it and published it in his 1903 work. It considers the principle of a rocket: a device that can apply an acceleration to itself (a thrust) by expelling part of its mass with high speed in the opposite direction, due to the conservation of momentum.

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