Orbit Insertion

Orbit insertion is the spaceflight operation of adjusting a spacecraft’s momentum, in particular to allow for entry into a stable orbit around a planet, moon, or other celestial body. This maneuver involves either deceleration from a speed in excess of the respective body’s escape velocity, or acceleration to it from a lower speed.

The result may also be a transfer orbit, there is e.g. the term descent orbit insertion. Often this is called orbit injection.

Read more about Orbit Insertion:  Deceleration, Acceleration, Alternatives To Rockets

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