• DocumentCode
    1728182
  • Title

    Laboratory tests for spacecraft charging and discharging: from Hertz, Millikan and de Broglie to today´s questions

  • Author

    Frederickson, A.R.

  • Author_Institution
    Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
  • Volume
    2
  • fYear
    2004
  • Abstract
    Hertz (1887) generated reasonably narrow-band radio frequency oscillations in metal dipoles using air discharges between the dipole elements. Nearly 50 years later technologists working with high voltage particle accelerators and gamma-irradiators noticed arc-discharge trees entirely inside solid insulating dielectrics (glass) stimulated by irradiation alone, without applied voltage. B. Gross et al. performed an early scientific study of the phenomena and related the onset of internal discharges to the quantity, in coulombs, of irradiation charge stopped inside the dielectric and held there for long time periods. Recent international studies have related the charge-induced electric field strength in the dielectric to the propagation of the internal discharge tree. When it exits a surface of the dielectric into vacuum, gas from the tree provides a conductive path across the vacuum. Higher conductivity is produced by higher quantities of gas. Whereas Hertz air arcs were low impedance, ≪70 Ohms, generating resonant responses, the irradiated unbiased dielectric arcs appear to be high-impedance, low-Q, phenomena. Recent researches address practical questions for spacecraft subjected to space radiations: (1) How many discharge trees are initiated in the dielectric per unit time? (2) How much electric current is conducted as a function of time? (3) What is the charge decay time constant in the dielectric? (4) Over spacecraft lifetimes, how is the charge distributed in the dielectric? (5) How does the initial dielectric discharge evolve to short out a HV power system? (6) How can discharges propagate along the vacuum surface of a dielectric? (7) How does the discharge current distribute among spacecraft electronic circuits. (8) Can a discharge burn out sensitive electronic devices and how can this be prevented?.
  • Keywords
    aerospace materials; dielectric materials; gamma-ray effects; spacecraft charging; surface charging; surface conductivity; trees (electrical); Hertz air arcs; charge decay time constant; charge distribution; charge-induced electric field strength; dielectric discharge; dielectric vacuum surface; electric current conductivity; internal discharge tree; irradiated unbiased dielectric arcs; laboratory tests; low impedance; space radiations; spacecraft charging effects; spacecraft discharging effects; spacecraft electronic circuits; spacecraft lifetimes; Dielectrics; Laboratories; Linear particle accelerator; Narrowband; Radio frequency; Space technology; Space vehicles; Surface discharges; Testing; Voltage;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Solid Dielectrics, 2004. ICSD 2004. Proceedings of the 2004 IEEE International Conference on
  • Print_ISBN
    0-7803-8348-6
  • Type

    conf

  • DOI
    10.1109/ICSD.2004.1350581
  • Filename
    1350581