• DocumentCode
    778231
  • Title

    Radiation Dosimeters Developed for SNAP 10A Flight Test

  • Author

    Kruse, W.G.

  • Author_Institution
    Lockheed Missiles & Space Company Sunnyvale, California
  • Volume
    13
  • Issue
    1
  • fYear
    1966
  • Firstpage
    230
  • Lastpage
    235
  • Abstract
    LMSC provided five sets of radiation dosimeters on the first SNAP 10A (reactor-thermoelectric converter) power system flight test to measure the reactor leakage radiations throughout the SNAPSHOT Agena orbital vehicle. Fast neutron and thermal neutron flux and gamma ray dose rate measurements were made. The radiation measurements were required for in flight analysis of the reactor steady state leakage radiation effects on the SNAPSHOT orbital power conversion, guidance, command and telemetry equipment. This solid state equipment was specially "radiation hardened" to withstand a year\´s exposure to the reactor radiations in the space environment. The paper covers a description of the dosimeters, principles of operation of each type of instrument, development, ground testing, calibration, vehicle integration and flight test results. Flight data of the reactor startup are presented in direct computer printout form showing the quality of the nuclear measurements obtained from the dosimeter orbital telemetry system. A brief description of the SNAPSHOT vehicle nuclear distributions developed from the flight measurements is also given.
  • Keywords
    Extraterrestrial measurements; Inductors; Neutrons; Nuclear measurements; Power measurement; Power system analysis computing; Power system measurements; Telemetry; Testing; Vehicles;
  • fLanguage
    English
  • Journal_Title
    Nuclear Science, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9499
  • Type

    jour

  • DOI
    10.1109/TNS.1966.4323969
  • Filename
    4323969