The three-stage Saturn V was designed to send a fully fueled CSM and LM to the Moon. It was 33 feet (10.1 m) in diameter and stood 363 feet (110.6 m) tall with its 96,800-pound (43,900 kg) lunar payload. Its capability grew to 103,600 pounds (47,000 kg) for the later advanced lunar landings. The S-IC first stage burned RP-1/LOX for a rated thrust of 7,500,000 pounds-force (33,400 kN), which was upgraded to 7,610,000 pounds-force (33,900 kN). The second and third stages burned liquid hydrogen, and the third stage was a modified version of the S-IVB, with thrust increased to 230,000 lbf (1,020 kN) and capability to restart the engine for translunar injection after reaching a parking orbit.
What did the second stage in the Saturn V end up doing?
burned liquid hydrogen burned liquid hydrogen burned liquid hydrogen burned liquid hydrogen burned liquid hydrogen
The second and third stages burned liquid hydrogen, and the third stage was a modified version of the S-IVB, with thrust increased to 230,000 lbf (1,020 kN) and capability to restart the engine for translunar injection after reaching a parking orbit.
The second and third stages burned liquid hydrogen, and the third stage was a modified version of the S-IVB, with thrust increased to two hundred thirty thousand lbf (ten twenty kN) and capability to restart the engine for translunar injection after reaching a parking orbit.
What did the second stage in the Saturn V end up doing?