• DocumentCode
    980245
  • Title

    Radiation Instrumentation Electronics for the Pioneers III and IV Space Probes

  • Author

    Josias, Conrad S.

  • Author_Institution
    Jet Propulsion Lab., California Institute of Technology, Pasadena, Calif.
  • Volume
    48
  • Issue
    4
  • fYear
    1960
  • fDate
    4/1/1960 12:00:00 AM
  • Firstpage
    735
  • Lastpage
    743
  • Abstract
    One of the devices carried aboard lunar payloads, Pioneer III and Pioneer IV, was a radiation measurement instrument. Its purpose was to detect and process information on particle flux rates encountered along the nominal cis-lunar trajectory to be followed by those payloads. Radiation data were collected by two different Geiger-Mueller tubes. One tube registered particle counts and the resultant accumulation was stored in a 17-stage scaler. The other tube provided average pulse current that was a compressed function of the counting rate. This current was fed to a resistor and the voltage thus formed was transferred to a telemetering subcarrier oscillator by way of a stable dc amplifier. The electronics discussed in this paper fall into three groups: 1) dc amplifier for the analog experiment, 2) high-voltage circuitry for the detectors, 3) digital circuitry for the counting experiment. Details of the encoding system, which permits a large dynamic range of counting rates to be clearly presented on a single subcarrier, are also discussed.
  • Keywords
    Circuits; Detectors; Instruments; Moon; Payloads; Probes; Pulse amplifiers; Pulse compression methods; Resistors; Voltage-controlled oscillators;
  • fLanguage
    English
  • Journal_Title
    Proceedings of the IRE
  • Publisher
    ieee
  • ISSN
    0096-8390
  • Type

    jour

  • DOI
    10.1109/JRPROC.1960.287476
  • Filename
    4066083