Rocketdyne H-1

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Invention

Domain

Science and technology

Knowledge cost

2

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What Wikipedia says

The Rocketdyne H-1 was a 205,000 lbf (910 kN) thrust liquid-propellant rocket engine burning LOX and RP-1. The H-1 was developed for use in the S-I and S-IB first stages of the Saturn I and Saturn IB rockets, respectively, where it was used in clusters of eight engines.

Excerpt from the Wikipedia article “Rocketdyne H-1”, under the CC BY-SA 4.0 license. Read the article on Wikipedia

Image: Taken by Jet Lowe, Public domain, via Wikimedia Commons.