• DocumentCode
    2558374
  • Title

    RTGs for space exploration at the end of the 20th century

  • Author

    Chmielewski, Art

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • fYear
    1989
  • fDate
    6-11 Aug 1989
  • Firstpage
    715
  • Abstract
    The use of radioisotope thermoelectric generators (RTGs) as energy conversion devices for spacecraft designed for weak-sunlight environments is discussed. The two upcoming missions Galileo and Ulysses will both use general-purpose heat source (GPHS) RTGs. Two other missions that are planned for the mid-nineties and will carry RTGs onboard are the comet rendezvous asteroid flyby (CRAF) and Cassini. Another mission that might become a program start in the last decade of the 20th century is Solarprobe, which is most likely to use modular RTGs. Several other missions that are in different planning stages that are in need of RTGs to meet their power requirements are the Mars rover sample return, planetary (Mars) penetrators, microspacecraft, and the Mars Egg. All of these missions are discussed, stressing their RTG requirements
  • Keywords
    space vehicle power plants; thermoelectric conversion; CRAF; Cassini; GPHS; Galileo; Mars Egg; Mars rover sample return; RTGs; Solarprobe; Ulysses; comet rendezvous asteroid flyby; energy conversion devices; general-purpose heat source; microspacecraft; planetary penetrators; radioisotope thermoelectric generators; spacecraft; Bills of materials; Earth; Gravity; Jupiter; Magnetic field measurement; Mars; Probes; Space exploration; Space vehicles; Venus;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Energy Conversion Engineering Conference, 1989. IECEC-89., Proceedings of the 24th Intersociety
  • Conference_Location
    Washington, DC
  • Type

    conf

  • DOI
    10.1109/IECEC.1989.74546
  • Filename
    74546