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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. Template:Saturn automobile timeline 1991 to 2010 - Wikipedia

    en.wikipedia.org/wiki/Template:Saturn_automobile...

    Main page; Contents; Current events; Random article; About Wikipedia; Contact us

  4. Saturn V instrument unit - Wikipedia

    en.wikipedia.org/wiki/Saturn_V_Instrument_Unit

    The last version, number 3, was 260 inches (6.6 m) in diameter and 36 inches (0.91 m) tall. It was designed by MSFC but manufactured by IBM in their factory at Huntsville, and flew on all Saturn IB and Saturn V launches.

  5. Apollo abort modes - Wikipedia

    en.wikipedia.org/wiki/Apollo_abort_modes

    During the first 42 seconds of flight for the Saturn V or 60 seconds of the flight for the Saturn IB, the rocket is still relatively upright and an abort is much like a pad abort, lasting up to 3,000 metres (9,800 ft). During the abort, the main pitch control motors move the CM out of the flight path of the possibly exploding rocket.

  6. Saturn V dynamic test vehicle - Wikipedia

    en.wikipedia.org/wiki/Saturn_V_Dynamic_Test_Vehicle

    The Saturn V dynamic test vehicle, designated SA-500D, is a prototype Saturn V rocket used by NASA to test the performance of the rocket when vibrated to simulate the shaking which subsequent rockets would experience during launch. It was the first full-scale Saturn V completed by the Marshall Space Flight Center (MSFC).

  7. 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).

  8. ST-124-M3 inertial platform - Wikipedia

    en.wikipedia.org/wiki/ST-124-M3_inertial_platform

    The ST-124-M3 inertial platform was a device for measuring acceleration and attitude of the Saturn V launch vehicle. It was carried by the Saturn V Instrument Unit, a 3-foot-high (0.91 m), 22-foot-diameter (6.7 m) section of the Saturn V that fit between the third stage (S-IVB) and the Apollo spacecraft. Its nomenclature means "stable table ...

  9. Timeline of Cassini–Huygens - Wikipedia

    en.wikipedia.org/wiki/Timeline_of_Cassini–Huygens

    View of Saturn from Cassini, taken in March 2004, shortly before the spacecraft's orbital insertion in July 2004. This article provides a timeline of the Cassini–Huygens mission (commonly called Cassini). Cassini was a collaboration between the United States' NASA, the European Space Agency ("ESA"), and the Italian Space Agency ("ASI") to send a probe to study the Saturnian system, including ...