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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. Propulsion and Structural Test Facility - Wikipedia

    en.wikipedia.org/wiki/Propulsion_and_Structural...

    The Propulsion and Structural Test Facility, also known as Building 4572 and the Static Test Stand, is a rocket testing facility of the George C. Marshall Space Flight Center in Huntsville, Alabama. Built in 1957, it was the site where the first single-stage rockets with multiple engines were tested. [ 4 ]

  4. Boilerplate (spaceflight) - Wikipedia

    en.wikipedia.org/wiki/Boilerplate_(spaceflight)

    The term boilerplate originated from the use of boilerplate steel [3] for the construction of test articles/mock-ups.Historically, during the development of the Little Joe series of 7 launch vehicles, there was only one actual boilerplate capsule and it was called such since its conical section was made of steel at the Norfolk Naval Shipyard.

  5. 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. [69] 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 [70] Nova was cancelled in 1964 and had reusable ...

  6. 1967 in spaceflight - Wikipedia

    en.wikipedia.org/wiki/1967_in_spaceflight

    Saturn V: LC-39A, Kennedy Space Center: NASA Apollo 4: NASA Highly elliptical orbit Test Saturn V and Apollo Command Module reentry: 9 November 20:37: Successful LTA-10R NASA Highly elliptical orbit Instrumented dynamic Simulation payload: 9 November: Successful Maiden flight of the Saturn V. LTA-10R remained attached to the S-IVB upper stage ...

  7. 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.

  8. Crawlerway - Wikipedia

    en.wikipedia.org/wiki/Crawlerway

    The Crawlerway was originally designed to support the weight of the Saturn V rocket and its payload, plus the Launch Umbilical Tower and mobile launcher platform, atop a crawler-transporter during the Apollo program. It was also used from 1981 to 2011 to transport the lighter Space Shuttles to their launch pads.

  9. Saturn V ELV - Wikipedia

    en.wikipedia.org/wiki/Saturn_V_ELV

    A 1968 proposal for a Saturn V ELV (MLV-SAT-V-25(S)U) According to the 1968 NASA document "Integrated Manned Interplanetary Spacecraft Concept Definition", there was a planned schedule for exploration under the ELV program. [2] After the first crewed Apollo lunar landing, NASA was hoping to progress through the following list: