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  <Observatory>
    <ResourceID>spase://SMWG/Observatory/DynamicsExplorer1</ResourceID>
    <ResourceHeader>
      <ResourceName>Dynamics Explorer 1</ResourceName>
      <AlternateName>1981-070A</AlternateName>
      <AlternateName>Explorer 62</AlternateName>
      <AlternateName>DE-A</AlternateName>
      <AlternateName>DE 1</AlternateName>
      <AlternateName>Dynamics Explorer-A</AlternateName>
      <ReleaseDate>2010-10-01T20:42:12Z</ReleaseDate>
      <Description>
          The Dynamics Explorer (DE) mission's general objective is to 
          investigate the strong interactive processes coupling the hot, 
          tenuous, convecting plasmas of the magnetosphere and the 
          cooler, denser plasmas and gases corotating in the earth's 
          ionosphere, upper atmosphere, and plasmasphere. Two 
          satellites, DE 1 and DE 2, were launched together and were 
          placed in polar coplanar orbits, permitting simultaneous 
          measurements at high and low altitudes in the same field-line 
          region. 
          
          The DE 1 spacecraft (high-altitude mission) uses an 
          elliptical orbit selected to allow 
          
          * (1) measurements extending 
          from the hot magnetospheric plasma through the plasmasphere to 
          the cool ionosphere; 
          * (2) global auroral imaging, wave 
          measurements in the heart of the magnetosphere, and crossing 
          of auroral field lines at several earth radii; and 
          * (3) measurements for significant periods along a magnetic field 
          flux tube. 
          
          The spacecraft approximated a short polygon 137 cm 
          in diameter and 115 cm high. The antennas in the X-Y plane 
          measured 200-m tip-to-tip, and on the Z-axis are 9 meters tip-
          to-tip. Two six-meter booms are provided for remote 
          measurements. Power is supplied by a solar cell array, mounted 
          on the side and end panels. The spacecraft is spin stabilized, 
          with the spin axis normal to the orbital plane, and the spin 
          rate at ten plus or minus 0.1 rpm. A pulse code modulation 
          (PCM) telemetry data system is used that operates in real time 
          or in a tape-recorder mode. Data have been acquired on a 
          science-problem-oriented basis, with closely coordinated 
          operations of the various instruments, both satellites, and 
          supportive experiments. Data acquired from the instruments are 
          temporarily stored on tape recorders before transmission at an 
          8:1 playback-to-record ratio. Additional operational 
          flexibility allows a playback-to-record ratio of 4:1. The 
          primary data rate is 16,384 bits per second. Since commands 
          are stored in a command memory unit, spacecraft operations are 
          not real time, except for the transmission of the wideband 
          analog data from the Plasma Wave Instrument (81-070A-02). 
          
          On October 22, 1990 science operations were terminated. On 
          February 28, 1991 Dynamics Explorer 1 operations were 
          offically terminated.
          
          Additional details may be found in R. A. 
          Hoffman et al., Space Sci. Instrum., v. 5, n. 4, p. 349, 1981. 
      </Description>
      <Contact>
        <PersonID>spase://SMWG/Person/Robert.A.Hoffman</PersonID>
        <Role>ProjectScientist</Role>
      </Contact>
      <InformationURL>
        <Name>NSSDC's Master Catalog</Name>
        <URL>http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=1981-070A</URL>
        <Description>Information about the Dynamics Explorer 1 mission</Description>
      </InformationURL>
    </ResourceHeader>
    <ObservatoryGroupID>spase://SMWG/Observatory/DE</ObservatoryGroupID>
    <Location>
      <ObservatoryRegion>Earth.NearSurface</ObservatoryRegion>
    </Location>
  </Observatory>
</Spase>
