Apollo applied the Oberth effect by placing its largest remaining burns near periapsis, the point in an orbit where the spacecraft moves fastest.
- On an elliptical orbit, speed is highest at periapsis and lowest at apoapsis. A burn at periapsis therefore buys more orbital energy per kilogram of propellant.
- The same principle applies to the departure and arrival geometry: burns timed when the spacecraft is moving fastest relative to the body it is leaving or approaching give the greatest velocity change for the propellant spent.
- This is why burn timing, not just burn size, appears in the mission plan: the trajectory is shaped so that the critical burns occur where the spacecraft is already moving quickly.
Key point: the Oberth effect turns timing into a fuel-saving tool. The propellant saved at periapsis is propellant that stays available for the return.