The complex mechanical choreography required to land humans on the Moon

How the Apollo Spacecraft works: Part 2 · 4:58 · Video: Jared Owen · Watch at the source

In short: A successful lunar mission was not a single flight, but a high-stakes sequence of separations, engine burns, and orbital maneuvers. From the massive Saturn V rocket to the delicate Lunar Module, every component played a precise role in ensuring the crew could reach the lunar surface and return safely.

The journey began with the Saturn V, a 363-foot-tall rocket weighing approximately 2.9 million kg at launch. This massive vehicle utilized three expendable stages to propel the spacecraft. The first stage, fueled by kerosene and liquid oxygen, propelled the rocket 42 miles upward before separating into the ocean. The second and third stages utilized liquid hydrogen and liquid oxygen to reach orbit and eventually push the spacecraft toward the Moon.

Once in space, the mission relied on three distinct spacecraft components. The Command Module, such as Columbia, served as the crew's primary habitat and was the only section designed to return to Earth. Attached to it was the Service Module, which provided essential life support, including oxygen, water, and power generated by fuel cells. This module also housed the main engine used for critical maneuvers like Lunar Orbit Insertion, which involved a second engine burn to adjust the orbit at a height of about 69 miles.

The Lunar Module (LM) was a two-stage vehicle consisting of a gold-and-black descent stage and a silver-and-black ascent stage. The descent stage used a rocket motor to slow the craft for a soft landing, while the ascent stage contained the pressurized crew compartment. After the landing, the ascent stage would ignite its engine to lift the astronauts back to the orbiting Command/Service Module. To ensure the mission's end, the descent stage remained on the Moon, while the ascent stage was programmed to crash into the lunar surface after docking.

Safety was maintained through specialized engineering, such as the Command Module's 'ablative' heat shield, which eroded during reentry to dissipate friction-induced heat. Following a tragic 1967 fire, the hatch design was updated from a 90-second opening process to a single hatch that could be opened in just five seconds using a pressurized nitrogen cylinder.

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