The Tsiolkovsky rocket equation, classical rocket equation, or ideal rocket equation is a mathematical equation that describes the motion of vehicles that follow the basic principle of a rocket: a device that can apply acceleration to itself using thrust by expelling part of its mass with high velocity can thereby move due to the conservation of momentum . Here, ->∆v is delta-v – the maximum change of velocity of the vehicle (with no external forces acting). ->m0 is the initial total mass, including propellant, also known as wet mass. ->mf is the final total mass without propellant, also known as dry mass. ->ve is the effective exhaust velocity. ->Isp is the specific impulse in dimension of time. ->g0 is the standard gravity . . Follow @atomstalk . . . #scienceeducation #equations #equation #rocketlaunch #rocketsofinstagram #rocketscience #rocketscientist #physicsstudent #astrophysicist #astrophysics https://www.instagram.com/p/CG_m0g8jXRG/?igshid=d8nf8zobv48s