• DocumentCode
    358541
  • Title

    Assessment of the Stirling power option for space science applications

  • Author

    Schreiber, Jeffrey G.

  • Author_Institution
    NASA Glenn Res. Center, Cleveland, OH, USA
  • Volume
    4
  • fYear
    2000
  • fDate
    2000
  • Firstpage
    39
  • Abstract
    Free-piston Stirling technology efforts in the past typically were intended to address power needs in the multi-kilowatt range. The Stirling power option was attractive primarily because of the high conversion efficiency and potential for long life. In recent years, several technology efforts have focused on the free-piston Stirling power convertor for space power applications, however the more recent efforts are intended to provide power at levels far below one kilowatt. Through a variety of projects funded by both NASA and DOE, the free-piston Stirling convertor technology has successfully demonstrated high efficiency and long life. Other areas of concern, such as control of multi-convertor systems, and vibration reduction have also been addressed. Efforts are being initiated to address issues such as EMI, radiation tolerance of organic materials, and the ability to operate through launch loads and survive with integrity. The status of the technology in these areas is briefly discussed
  • Keywords
    Stirling engines; power convertors; radioisotope thermoelectric generators; space vehicle power plants; EMI; Stirling power convertor; Stirling power option; free-piston Stirling technology; high conversion efficiency; multi-convertor systems control; organic materials; radiation tolerance; radioisotope heat source; space science applications; vibration reduction; Converters; Interference; NASA; Optical refraction; Power system dynamics; Power systems; Radioactive materials; Space missions; Space technology; US Department of Energy;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference Proceedings, 2000 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-5846-5
  • Type

    conf

  • DOI
    10.1109/AERO.2000.878363
  • Filename
    878363