• DocumentCode
    3219397
  • Title

    Space power technology

  • Author

    Rose, M. Frank

  • Author_Institution
    Space Power Inst., Auburn Univ., AL, USA
  • fYear
    1996
  • fDate
    25-27 Jun 1996
  • Firstpage
    9
  • Lastpage
    14
  • Abstract
    The trends today are toward smaller satellites with increased capability. These two trends place enormous demands on the technology used to power such space systems. Typical power sources are nuclear, photovoltaic, and chemical. As the power available on a typical satellite decreases, the use of long pulsed power sources becomes more attractive. Technologies such as electrochemical capacitors, pulsed batteries and flywheels offer the possibility of employing high power subsystems for limited times without undue burden on the spacecraft power train. The state of the art in each of the pulsed storage devices is discussed and preliminary experiments described which use an electrochemical power source to power a spacecraft propulsion unit such as an arc-jet or Hall effect thruster
  • Keywords
    aerospace engines; aerospace propulsion; energy storage; pulsed power technology; space vehicle power plants; Hall effect thruster; arc-jet; electrochemical capacitors; flywheels; pulsed batteries; pulsed power sources; pulsed storage devices; satellites; space power technology; spacecraft power train; spacecraft propulsion unit; state of the art; Batteries; Capacitors; Chemical technology; Flywheels; Photovoltaic systems; Propulsion; Satellites; Solar power generation; Space technology; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Power Modulator Symposium, 1996., Twenty-Second International
  • Conference_Location
    Boca Raton, FL
  • Print_ISBN
    0-7803-3076-5
  • Type

    conf

  • DOI
    10.1109/MODSYM.1996.564436
  • Filename
    564436