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The C-5 was confirmed as NASA's choice for the Apollo program in early 1962, and was named the Saturn V. [31] [32] The C-1 became the Saturn I and C-1B became Saturn IB. [32] Von Braun headed a team at the MSFC to build a vehicle capable of launching a crewed spacecraft to the Moon. [ 33 ]
Description: The Saturn V was the launch vehicle for all twelve Apollo missions and also the sole Skylab mission. This is the third stage of one of only three complete Saturn V rockets to exist and which consists of the following components:- 1st stage ‘S-IC-14’ from SA-514, which was planned to fly on Apollo 19. 2nd stage ‘S-II-15’ from SA-515, which was planned to fly on Apollo 20 ...
J002E3 is an object in space which is thought to be the S-IVB third stage of the Apollo 12 Saturn V rocket. It was discovered on September 3, 2002, by amateur astronomer Bill Yeung . Initially thought to be an asteroid , it has since been tentatively identified as the third stage of Apollo 12 Saturn V based on spectrographic evidence consistent ...
The Saturn C-5 (later given the name Saturn V), the most powerful of the Silverstein Committee's configurations, was selected as the most suitable design. At the time the mission mode had not been selected, so they chose the most powerful booster design in order to ensure that there would be ample power. [ 24 ]
The S-II (pronounced "S-two") was the second stage of the Saturn V rocket. It was built by North American Aviation. Using liquid hydrogen (LH2) and liquid oxygen (LOX) it had five J-2 engines in a quincunx pattern. The second stage accelerated the Saturn V through the upper atmosphere with 1,000,000 pounds-force (4.4 MN) of thrust.
S-IC-T was planned as a test rocket only and not to be used in the later Apollo program. The Saturn V rocket was used in the Apollo program to depart Earth's gravity. S-IC-T, like all following Saturn V's S-IC rockets used five Rocketdyne F-1 engines. The Rocketdyne F-1 engine was first tested in March 1959 and delivered to NASA in October 1963.
The Saturn V rocket used by Apollo 8 was designated AS-503, or the "03rd" model of the Saturn V ("5") rocket to be used in the Apollo-Saturn ("AS") program. When it was erected in the Vehicle Assembly Building on December 20, 1967, it was thought that the rocket would be used for an uncrewed Earth-orbit test flight carrying a boilerplate ...
Launch Complex 39B was designed to handle launches of the Saturn V rocket, the largest and most powerful launch vehicle, which would propel Apollo spacecraft to the Moon. Launch Complex 39B's inaugural launch in May 1969 was also that of the only Saturn V to launch from the pad; SA-505, used to launch the Apollo 10 mission.