The fuel used is liquid hydrogen with liquid oxygen as an oxidizer. It has five Rocketdyne J-2 rocket engines that can provide 4900 kN of thrust.
It is 25 meters tall and 10 meters wide, similar to the previous stage, and weighs over 480 tons when fully fueled. The S-II is the second stage of the Saturn V.
The first stage can bring the rocket to a suborbital trajectory that cannot leave the atmosphere. The fuel used on this stage is RP-1 with liquid oxygen as an oxidizer. It is powered by five Rocketdyne F1 engines that can provide 34 thousand kilonewtons of thrust. It is 42 meters tall and ten meters wide and weighs over 2300 tons when fully fueled. The S-IC is the first stage of the Saturn V. 2.1 All of the missions which was used by the Saturn V.
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