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Rocket, Third Stage, S-IVB-D Dynamic Test Vehicle, Saturn V

Air and Space Museum

There are restrictions for re-using this image. For more information, visit the Smithsonian's Terms of Use page .
International media Interoperability Framework
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    Object Details

    Manufacturer

    McDonnell Douglas Corporation

    Summary

    This is the S-IVB-D, or third stage of the Dynamic Test version of the Saturn V. This stage of the rocket was not meant to fly but was used for ground tests pior to the actual flight tests. As in the flyable version of the Saturn V, the stage shown here is fitted with one J-2 rocket engine, although it was inoperable. The Dynamic Test version of the rocket was extremely important in Apollo program - it proved the validity of the vehicle's structural design. In its flyable form, the 363-foot long, 33-foot diameter operational version of the Saturn V rocket took a dozen astronauts toward the Moon during 1969-1972 and is considered one of the greatest engineering achievements in history. The third stage was transferred to from NASA to the Smithsonian in 1975.

    Credit Line

    Transferred from the National Aeronautics and Space Administration

    Inventory Number

    A19750677000

    Restrictions & Rights

    Usage conditions apply

    Type

    CRAFT-Missile & Rocket Parts

    Materials

    Aluminum skin; stainless and other steels in single J-2 engine.

    Dimensions

    Length, 56 feet; diameter, 33 feet

    Country of Origin

    United States of America

    See more items in

    National Air and Space Museum Collection

    Data Source

    National Air and Space Museum

    Metadata Usage

    Not determined

    Link to Original Record

    http://n2t.net/ark:/65665/nv981eaf25a-8bde-4401-a08d-33b78a105704

    Record ID

    nasm_A19750677000

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