You are ready to go: calculate velocity at burnout (max velocity, v), boost phase distance yb, and coast phase distance yc (you will sum these last two for total altitude). note that "g" is acceleration of gravity in metric units = 9.8.. Burnout velocity of a double 2-stage rocket to calculate the burnout velocity of a single stage rocket we need to have the total mass of the double 2 stage rocket in kilograms. we also need, the specific impulse of the double stage rocket in seconds (s).. The velocity of a rocket at the time when depletion of the fuel or oxidant occurs. also known as all-burnt velocity; burnt velocity. the maximum velocity achieved by a rocket or missile at the termination of burning of propellant. the rocket or missile starts decelerating from this point. want to.
The tsiolkovsky rocket equation, classical rocket equation, or ideal rocket equation, 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 and thereby move due to the conservation of momentum.. the equation relates the delta-v (the maximum change of velocity of. Rocket equations mr = rocket mass in kg me = engine mass (including propellant) in kg mp = propellant mass in kg a = acceleration m/s2 f = force in kg . m/s2 g = acceleration of gravity = 9.81 m/s2 v
