Apollo 11: the physics behind the Moon landing — and its gaps

Reentries at 11 km/s, a 45-ton spacecraft and a risk ratio 4.5 times higher: the data that supports — and the data that doesn't — the Apollo program.

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Apollo 11: the physics behind the Moon landing — and its gaps
Apollo 11: the data that supports the Moon landing, and the data that doesn't

Did men walk on the Moon in July 1969, or was it all a cardboard set with aluminum foil and low-gravity hops? The doubt resurfaces every time someone digs up a video from the Apollo program — the latest, showing the Apollo 12 launch with surprisingly good image quality — and compares it with what the industry seems unable to repeat today. The question can be answered badly with YouTube videos, or considerably better with physics, tonnage and accident statistics.

Reentries at 11 km/s: the physics that allows no narrative

The most repeated argument is that the Apollo capsules fell like projectiles, on a ballistic trajectory impossible to survive. The premise is false from the start: the spacecraft entered the atmosphere directly and could travel up to 1,500 nautical miles from the entry point before splashdown. The difference in speeds is the other fact that dismantles half-truths. The Apollos that went to the Moon reentered at about 11 km/s; Apollo 7 and 9, which never left Earth orbit, did so at 8 km/s. The physics is the same used today and the numbers are on the table, but they demand more patience than a three-line headline.

45 tons versus 7.2: why Apollo can't be compared to the Soyuz

The command and service module plus the lunar module weighed 45 tons combined. The Soyuz MS, the modern version, comes in at around 7.2. That's the gap between putting something into Earth orbit and escaping it. That's why the missions aren't interchangeable and why the program was built in steps: Apollo 4 in November 1967, first full unmanned flight of the Saturn V; Apollo 5 in January 1968, lunar module in Earth orbit; Apollo 7 in October '68, first crewed mission; Apollo 8 in December, orbiting the Moon; Apollo 9 in March '69, crewed lunar module. Each step, before the next.

The risk ratio that sneaks into every comparison

Here the ground gets swampy. The statistical risk factor of the Apollo missions was 4.5 times that of the Space Shuttle, a figure waved around to ridicule any claim of technical superiority. But everything depends on the denominator: if you take the Apollo 1 fire out of the statistics, the result flips. Between 1961 and 1971 NASA lost 8 astronauts — five in training accidents and three in ground tests — versus 5 Soviet cosmonauts. In mission flights, 0 Americans died versus 4 Soviets. The Shuttle flew 135 missions and lost 14 crew members in Challenger and Columbia. The full breakdown, mission by mission, is out there and dismantles more than one convenient version.

From Saturn-Shuttle to the lunar rover: doubts with documented answers

Where did the lunar rover go if the module was tiny? Folded up, like almost everything in aerospace engineering. Why was the Saturn abandoned? Money: in 1971-1972 it was estimated that reviving the F-1 engines, complex and partly handcrafted, cost more than the solid-fuel line that ended up powering the Shuttle. A Shuttle mounted on the first stage of a Saturn V was even studied, and rejected. Losing blueprints for specific parts is a classic of any industrial program shut down in a hurry, not proof of anything.

A million and a half jobs over fifteen years; subcontractors like Motorola, Bell Aerosystems, Westinghouse or Pratt & Whitney. If it was all a set, it was built with a level of production that quite a few current blockbusters would envy. And we're still arguing about whether some men in aluminum suits stepped on gray dust.

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Summary of a discussion on Burbuja.info - Foro de economía, actualidad y política., translated from Spanish and reviewed before publication. Read the full discussion (96 replies).

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