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  2. Saturn V - Wikipedia

    en.wikipedia.org/wiki/Saturn_V

    The Saturn V reached 400 feet per second (120 m/s) at over 1 mile (1,600 m) in altitude. Much of the early portion of the flight was spent gaining altitude, with the required velocity coming later. The Saturn V broke the sound barrier at just over 1 minute at an altitude of between 3.45 and 4.6 miles (5.55 and 7.40 km). At this point, shock ...

  3. Saturn (rocket family) - Wikipedia

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

    Three variants of the Saturn family which were developed: Saturn I, Saturn IB, and Saturn V The Saturn family of American rockets was developed by a team of former German rocket engineers and scientists led by Wernher von Braun to launch heavy payloads to Earth orbit and beyond.

  4. Super heavy-lift launch vehicle - Wikipedia

    en.wikipedia.org/wiki/Super_heavy-lift_launch...

    The American Saturn MLV family of rockets was proposed in 1965 by NASA as successors to the Saturn V rocket. [71] It would have been able to carry up to 160,880 kg (354,680 lb) to low Earth orbit. The Nova designs were also studied by NASA before the agency chose the Saturn V in the early 1960s [ 72 ] Nova was cancelled in 1964 and had reusable ...

  5. S-IC - Wikipedia

    en.wikipedia.org/wiki/S-IC

    The S-IC (pronounced S-one-C [3] [4]) was the first stage of the American Saturn V rocket. The S-IC stage was manufactured by the Boeing Company. Like the first stages of most rockets, more than 90% of the mass at launch was propellant, in this case RP-1 rocket fuel and liquid oxygen (LOX) oxidizer.

  6. S-IC-T - Wikipedia

    en.wikipedia.org/wiki/S-IC-T

    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.

  7. 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.

  8. 1973 in spaceflight - Wikipedia

    en.wikipedia.org/wiki/1973_in_spaceflight

    Saturn V: Kennedy LC-39A: NASA: Skylab: NASA: Low Earth Space Station: 11 July 1979: Successful First American Space Station Last flight of the Saturn V rocket Damaged during launch, but repaired 16 May 16:40 Titan IIIB (24B) Vandenberg SLC-4W: OPS 2093 NRO / US Air Force: Low Earth Reconnaissance: 13 June 1973: Successful 17 May 13:19 Kosmos ...

  9. Kennedy Space Center Launch Complex 39B - Wikipedia

    en.wikipedia.org/wiki/Kennedy_Space_Center...

    Launch Complex 39B (LC-39B) is the second of Launch Complex 39's three launch pads, located at NASA's Kennedy Space Center in Merritt Island, Florida. The pad, along with Launch Complex 39A , was first designed for the Saturn V launch vehicle, which at the time was the United States' most powerful rocket.