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  2. Saturn-Shuttle - Wikipedia

    en.wikipedia.org/wiki/Saturn-Shuttle

    The Shuttle would handle space station logistics, while the Saturn V would launch components. This would have allowed the International Space Station, using a Skylab or Mir configuration with both U.S. and Russian docking ports, to have been lifted with just a handful of launches. However, it was ultimately rejected on basis of cost.

  3. Comparison of orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    This comparison of orbital launch systems lists the attributes of all current and future individual rocket configurations designed to reach orbit. A first list contains rockets that are operational or have attempted an orbital flight attempt as of 2024; a second list includes all upcoming rockets.

  4. Saturn V - Wikipedia

    en.wikipedia.org/wiki/Saturn_V

    Arthur Rudolph became the project director of the Saturn V rocket program in August 1963. He developed the requirements for the rocket system and the mission plan for the Apollo program. The first Saturn V launch lifted off from Kennedy Space Center and performed flawlessly on November 9, 1967, Rudolph's birthday. [40]

  5. Comparison of orbital rocket engines - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    Space Shuttle, Orion, Apollo CSM: Active Upper ... Saturn V: Retired 1st ... 5.97: Space Shuttle Solid Rocket Booster [k]

  6. Rocketdyne F-1 - Wikipedia

    en.wikipedia.org/wiki/Rocketdyne_F-1

    Wernher von Braun with the F-1 engines of the Saturn V first stage at the U.S. Space and Rocket Center. Rocketdyne developed the F-1 and the E-1 to meet a 1955 U.S. Air Force requirement for a very large rocket engine. The E-1, although successfully tested in static firing, was quickly seen as a technological dead-end, and was abandoned for the ...

  7. Comparison of crewed space vehicles - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_crewed_space...

    Saturn IB Saturn V: 3: 8.5: 3.91: 5,500 CM + 14,700 LM + 24,500 Service Module: Fuel cells Parachute splashdown (two drogues, three pilots, three mains) 1967 (1966) 1975: 15 (4) [note 3] Space Shuttle orbiter USA: Rockwell International: LEO: Space Shuttle: 8 [note 4] 37.24: 4.8 [note 5] 109,000: Fuel cells Runway landing (with one pilot and ...

  8. Launch status check - Wikipedia

    en.wikipedia.org/wiki/Launch_status_check

    For Space Shuttle missions, in the firing room at the Launch Control Center, the NASA Test Director (NTD) performed this check via a voice communications link with other NASA personnel. The NTD was the leader of the shuttle test team responsible for directing and integrating all flight crew, orbiter, external tank/solid rocket booster and ...

  9. 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 ...