Apollo 11 · The Lunar Module · Chapter 3 of 7

How Landing Worked

Landing required controllable thrust, contact sensors and shock-absorbing legs.

Chapter 03 / 07 · Chapter 3

The descent engine

My main descent engine was a deep-throttling, ablative rocket mounted on a gimbal beneath the descent stage. It could produce approximately 45,000 newtons of maximum thrust, or about 10,125 pounds-force. Deep throttling means the engine could vary its thrust over a wide range, helping the astronauts control their descent. The gimbal allowed the thrust direction to be adjusted.

What powered the engine?

  • Aerozine 50 was the fuel.
  • Nitrogen tetroxide was the oxidizer.
  • The propellants were stored separately and combined in the engine to produce thrust.

How I sensed the ground

Contact probes extended below three landing footpads. When a probe touched the lunar surface, it provided a contact signal to the crew and helped Armstrong know when the spacecraft had reached the ground.

How I absorbed impact

My landing legs incorporated crushable aluminium honeycomb shock absorbers. During touchdown, the honeycomb could deform and absorb some landing energy. The footpads helped distribute my weight.

A soft landing is a controlled touchdown in which a spacecraft reduces its speed enough to reach the surface without a destructive impact. It does not mean zero impact; it means the impact is managed so the vehicle can survive.

Mission details are based on the NASA/NSSDCA Apollo 11 Lunar Module / EASEP record supplied for this project.