Explorer 14

      Explorer 14
      Explorer 14 mock-up.jpg
      Operator NASA
      Major contractors Goddard Space Flight Center
      Launch date October 2, 1962
      Launch vehicle Thor-Delta
      COSPAR ID 1962-051A
      Homepage NASA NSSDC Master Catalog
      Mass 40kg
      Orbital elements
      Eccentricity 0.839
      Inclination 42.8°
      Apoapsis 96189.0 km
      Periapsis 2601.0 km
      Orbital period 2184.6 minutes

      Explorer 14 is a spin-stabilized, solar-cell-powered spacecraft instrumented to measure cosmic-ray particles, trapped particles, solar wind protons, and magnetospheric and interplanetary magnetic fields. A 16-channel PFM/PM time-division multiplexed telemeter was used. The time required to sample the 16 channels (one frame period) was 0.323 s. Half of the channels were used to convey eight-level digital information, and the others were used for analog information. During ground processing of the telemetered data, the analog information was digitized with an accuracy of 1/100th of full scale. One analog channel was subcommutated in a 16-frame-long pattern and was used to telemeter spacecraft temperatures, power system voltages, currents, etc. A digital solar aspect sensor measured the spin period and phase, digitized to 0.041 s, and the angle between the spin axis and sun direction to about 3-deg intervals.[1][2]

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      Last modified on 4 May 2013, at 05:18