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Rocket, Solid Fuel, Test Vehicle, Little Joe II

Air and Space Museum

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International media Interoperability Framework
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    Object Details

    Manufacturer

    General Dynamics Corp., Convair Division

    Summary

    The Little Joe II is a solid-propellant rocket for launching Project Apollo "boilerplate" space capsules on tests of the Launch Escape System (LES). The LES consisted of a tower with solid-fuel rockets to pull the Apollo Command Module off the launch vehicle, plus aBoost Protective Cover over the Command Module. Five Little Joe II vehicles were flown from 1963 to 1966, simulating various launch emergencies on Apollo-Saturn rockets that required the LES to pull the Command Module and its crew away from the failing booster. All were launched at the White Sands Missile Range, New Mexico, and all were successful. The concept was based on the earlier Little Joe rocket NASA had used to test the Mercury capsule’s escape tower.
    NASA transferred this Little Joe II to the Smithsonian Institution in 1974.

    Credit Line

    Transferred from the National Aeronautics and Space Administration

    Inventory Number

    A19740926000

    Restrictions & Rights

    Usage conditions apply

    Type

    CRAFT-Missiles & Rockets

    Materials

    Body, overall, corrugated aluminum panels

    Dimensions

    Overall: 1034 3/8 in. long x 153 5/8 in. diameter x 324 in. span (2627.38 x 390.14 x 822.96cm)

    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/nv9d1aa7987-0a2d-4fde-b308-57258c9d9f8c

    Record ID

    nasm_A19740926000

    Discover More

    Rockets and Missiles

    Image of F-1 rocket engine cluster on display

    Rockets and Missiles

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