Orbital Maneuver - General - Rocket Equation

Rocket Equation

The Tsiolkovsky rocket equation, or ideal rocket equation is an equation that is useful for considering vehicles that follow the basic principle of a rocket: where a device that can apply acceleration to itself (a thrust) by expelling part of its mass with high speed and moving due to the conservation of momentum. Specifically, it is a mathematical equation that relates the delta-v (the maximum change of speed of the rocket if no other external forces act) with the effective exhaust velocity and the initial and final mass of a rocket (or other reaction engine.)

For any such maneuver (or journey involving a number of such maneuvers):

where:

is the initial total mass, including propellant,
is the final total mass,
is the effective exhaust velocity ( where is the specific impulse expressed as a time period and is the gravitational constant),
is delta-v - the maximum change of speed of the vehicle (with no external forces acting).

Read more about this topic:  Orbital Maneuver, General

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