Just for viewing purposes. You can store and calculate this formula only inside the application.
ideal rocket equation
/*Speed of an ideal rocket */ v = v_e* LN(m_0/m_r)
This formula describes the velocity of an (ideal) rocket after burning m1-m units of fuel with a starting velocity of 0. m_0: initial mass of rocket, including fuel. m_r: remaining mass v_exh: speed of exhaust when leaving the rocket