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  2. Saturn V - Wikipedia

    en.wikipedia.org/wiki/Saturn_V

    In the time frame from 1969 to 1971 the cost of launching a Saturn V Apollo mission was between $185,000,000 to $189,000,000, [1 ... Apollo 17 S-IVB rocket stage, ...

  3. Apollo 17 - Wikipedia

    en.wikipedia.org/wiki/Apollo_17

    Originally planned to launch on December 6, 1972, at 9:53 p.m. EST (2:53 a.m. on December 7 UTC), [65] Apollo 17 was the final crewed Saturn V launch, and the only one to occur at night. The launch was delayed by two hours and forty minutes due to an automatic cutoff in the launch sequencer at the T−30 second mark in the countdown.

  4. List of Apollo missions - Wikipedia

    en.wikipedia.org/wiki/List_of_Apollo_missions

    Apollo 6: Saturn V SA-502 April 4, 1968, 16:12 GMT Launch Complex 39A. Second flight of Saturn V; severe "pogo" vibrations caused two second-stage engines to shut down prematurely, and third stage restart to fail. SM engine used to achieve high-speed re-entry, though less than Apollo 4. NASA identified vibration fixes and declared Saturn V man ...

  5. Rocketdyne F-1 - Wikipedia

    en.wikipedia.org/wiki/Rocketdyne_F-1

    The engine uses a gas-generator cycle developed in the United States in the late 1950s and was used in the Saturn V rocket in the 1960s and early 1970s. Five F-1 engines were used in the S-IC first stage of each Saturn V, which served as the main launch vehicle of the Apollo program.

  6. Saturn (rocket family) - Wikipedia

    en.wikipedia.org/wiki/Saturn_(rocket_family)

    Saturn V – 13 launches; the Moon rocket that sent Apollo astronauts to the Moon, and carried the Skylab space station into orbit. Built members of the Saturn family A Saturn I ( SA-1 ) liftoff from LC-34

  7. Apollo program - Wikipedia

    en.wikipedia.org/wiki/Apollo_program

    A Saturn V rocket launches Apollo 11, 1969. Saturn V launch vehicles and flights were designated with an AS-500 series number, "AS" indicating "Apollo Saturn" and the "5" indicating Saturn V. [67] 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 ...

  8. S-IVB - Wikipedia

    en.wikipedia.org/wiki/S-IVB

    The S-IVB (pronounced "S-four-B") was the third stage on the Saturn V and second stage on the Saturn IB launch vehicles. Built by the Douglas Aircraft Company , it had one J-2 rocket engine. For lunar missions it was fired twice: first for Earth orbit insertion after second stage cutoff, and then for translunar injection (TLI).

  9. SA-500F - Wikipedia

    en.wikipedia.org/wiki/SA-500F

    SA-500F was the first complete assembly of something resembling a Saturn V, and model makers quickly patterned their designs after its paint scheme, but engineers changed the black stripe to white in the intertank section of the first stage for flight vehicles after discovering the intertank got too hot from the heat of the Sun. The third stage ...