• DocumentCode
    906428
  • Title

    Cosmic Ray Neutron Monitor for OGO-F

  • Author

    Lockwood, John A. ; Chupp, Edward L. ; Jenkins, Robert W.

  • Author_Institution
    Department of Physics, University of New Hampshire, Durham, N. H. 03824
  • Volume
    7
  • Issue
    2
  • fYear
    1969
  • fDate
    4/1/1969 12:00:00 AM
  • Firstpage
    88
  • Lastpage
    93
  • Abstract
    The objective of this experiment is to monitor the cosmic-ray neutron flux over a large region of space near the earth for an extended time with a simple neutron monitor. The basic detecting system to measure the integrated neutron flux from 10-8 to 15 MeV consists of a moderated He3 proportional counter surrounded by a charged-particle rejection system. A plastic scintillator viewed by a photomultiplier is operated in coincidence with the neutron counter to determine the energy spectrum and flux in the 1-10 MeV range. In order to minimize contributions from neutrons produced within the OGO spacecraft, the sensor is located about 4.5 meters out on the EP-5 boom. The experiment includes an in-flight calibrator to check pulse discriminator levels on neutron and charged-particle channels and a calibration-loop system to compensate for changes in the photo-multiplier gain. The mean neutron detection efficiency for the expected neutron energy spectrum over the energy range 10-8-15 MeV is 1.8 cm2. The weight of the neutron sensor is 2.58 kg, with a length of 0.314 meter and a diameter of 0.111 meters. The total power requirements are 4.5 watts.
  • Keywords
    Acoustic noise; Atmosphere; Atmospheric measurements; Impedance; Magnetic flux; Magnetosphere; Monitoring; Neutrons; Resonance; Space vehicles;
  • fLanguage
    English
  • Journal_Title
    Geoscience Electronics, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9413
  • Type

    jour

  • DOI
    10.1109/TGE.1969.271327
  • Filename
    4043323