• DocumentCode
    1230076
  • Title

    SNAP-8 Electrical System

  • Author

    Nice, A.W. ; Bradley, S.L.

  • Author_Institution
    National Aeronautics and Space Administration Lewis Research Center
  • Volume
    2
  • Issue
    2
  • fYear
    1964
  • fDate
    4/1/1964 12:00:00 AM
  • Firstpage
    867
  • Lastpage
    873
  • Abstract
    This paper presents a brief description of the SNAP-8 electrical-system design changes and provides a broad perspective of the overall system changes incorporated early in 1963. These modifications made feasible a modular approach to component and subsystem development, provided greater system development flexibility, and permitted the application of much presently available electrical technology. The rotating speed was changed from 20,000 to 12,000 revolutions per minute (rpm) resulting in a change of system frequency from 1,000 to 400 cycles per second (cps). The alternator and the regulator were removed from the high-temperature and mercury-vapor environment. The mercury lubrication and cooling concept was replaced with organic-fluid lubrication and a low-temperature cooling loop was added to the system. Significant development problems still exist, however. There remains the requirement for 10,000-hours minimum life in the space and nuclear environment, coupled with extremely high reliability objectives.
  • Keywords
    Alternators; Coolants; Cooling; Electromagnetic heating; Frequency; Heat pumps; Heat transfer; Inductors; Lubrication; Space heating;
  • fLanguage
    English
  • Journal_Title
    Aerospace, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0536-1516
  • Type

    jour

  • DOI
    10.1109/TA.1964.4319677
  • Filename
    4319677