Saturn V second stage rocket engines

Saturn V second stage rocket engines
Kennedy Space Center, Florida (FL), US
The S-II is the second stage of the Saturn V rocket built by North American Aviation. It used liquid hydrogen and liquid oxygen. The Saturn V had five J-2 engines. The second stage developed 1,000,000 pounds-force of thrust.
The S-II is the second stage of the Saturn V rocket built by North American Aviation. It used liquid hydrogen and liquid oxygen. The Saturn V had five J-2 engines. The second stage developed 1,000,000 pounds-force of thrust.
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Links: en.wikipedia.org
By: kjfitz

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