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    Sputnik 3 (, Satellite 3) was a Soviet satellite launched on May 15, 1958 from Baikonur cosmodrome by a modified R-7/SS-6 ICBM. It was a research satellite to explore the upper atmosphere and the near space. Due to a hardware failure of its tape recorder, the satellite failed to detect the Van Allen radiation belt.

    In July 1956, the Soviet Union's OKB-1 drafted a project to design and build the first Earth satellite, designated ISZ (Artificial Earth Satellite). Sputnik 3 was planned to be the first satellite launched by the Soviet Union. The new R-7 intercontinental ballistic missile was ready to launch before Sputnik 3 was ready. The Sputnik 3 completion date kept slipping and Sergi Korolev substituted the relatively simple Sputnik 1 as the first satellite to be launched, instead. The Sputnik 2 was also ready earlier and launched earlier than Sputnik 3. Korolev was concerned that if he waited for Sputnik 3 to be ready, the United States would be the first to launch an artificial satellite.

    Sputnik 3 was an automatic scientific laboratory spacecraft. It was conically shaped and was 3.57 m long and 1.73 m wide at its base. It weighed 1,327 kg. The scientific instrumentation (twelve instruments) provided data on pressure and composition of the upper atmosphere, concentration of charged particles, photons in cosmic rays, heavy nuclei in cosmic rays, magnetic and electrostatic fields, and meteoric particles. The outer radiation belts of the Earth were detected during the flight. Its tape recorder failed, so it could not map the Van Allen radiation belt. The spacecraft remained in orbit until April 6, 1960, when the orbit degraded from drag in upper atmosphere to the point causing the satellite to enter the atmosphere.


        Sputnik 3
            See also
    Class"toccolours" border="1" c...
    NameSputnik III
    image
    OrganizationSoviet Union
    Major ContractorsKorolev Design Bureau
    Mission TypeEarth Science
    Satellite OfEarth
    LaunchMay 15, 1958 at 07:12:00 Coordinated Univer...
    Launch VehicleSapwood SS-6 8K71PS
    DecayApril 6, 1960
    Mission Duration692 days
    Mass1,327 kg
    Nssdc Id1958-004B
    Webpagehttp://nssdc.gsfc.nasa.gov/database/MasterCat...
    Orbital Elementsyes
    Semimajor Axis7418.7 km
    Eccentricity.110932
    Inclination65.18°
    Orbital Period105.9 minutes
    Apoapsis1,864 km
    Periapsis217 km
    Orbits~10,000
    Class"toccolours" border="1" c...
    - Align"center" !colspan="2" cel...

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    Scientus.org Dictionary (Yet Another Wiki) RC : 1.39
    This article is licensed under the GNU Free Documentation License [copyleft]. It uses material from the Wikipedia article "Sputnik 3". link