Skip to main content

A System for Measuring and Controlling the Surface Potential of Rockets Flown in the Ionosphere

  • Conference paper
Photon and Particle Interactions with Surfaces in Space

Part of the book series: Astrophysics and Space Science Library ((ASSL,volume 37))

Abstract

A short account is given of the effects on rocket potential of drawing excessive electron currents to Langmuir probes mounted on a rocket. A system is described whereby the rocket to plasma potential can be regulated by means of ejecting electrons into the plasma medium with an electron gun which is servo-controlled. The system was developed and tested in a laboratory plasma, simulating ionospheric conditions, and was consequently incorporated in a rocket payload P119H which reached an apogee of about 140 km. The results presented show the extent to which rocket potential can change as a consequence of the various currents drawn to the probes when no regulation is applied and also the high degree of regulation attained when the control system is brought into operation. Certain improvements, which can be made to the system in order to avoid gross contact potential difference effects, are suggested.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 39.99
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 54.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

References

  • Boyd, R. L. F.: 1968, in Lochte-Holtgreven (ed.), Plasma Diagnostics, Chapt. 12, North Holland Pub. Co., Amsterdam.

    Google Scholar 

  • Blanquart, P. and Ramond, J.: 1966, L’Echo des Recherches, No. 45. (1966)

    Google Scholar 

  • De Barr, A. E.: 1962 Automatic ControlChapt. 2, Reinhold Pub. Co.

    Google Scholar 

  • Goodall, C. V.: 1971, Planetary Space Sci. 19, 827.

    Article  ADS  Google Scholar 

  • Huang, F. T.: 1970, Ph.D. Thesis, Maryland University, U.S.A. (1970)

    Google Scholar 

  • Laframboise, J. G.: 1966, Univ. of Toronto Inst. for Aerospace Stud. Report No. 100, Canada. Mott-Smith, H. M. and Langmuir, I.: 1926, Phys. Rev. 28, 727.

    Google Scholar 

  • Polychronopulos, B.: 1970, M.Sc. Thesis, Birmingham University, U.K.

    Google Scholar 

  • Sayers, J.: 1970 J. Atmospheric Terrest. Phys. 32663.

    Google Scholar 

  • Swift, J. D. and Schwar, M. J. R.: 1970, Electrical Probes for Plasma Diagnostics,Chapt. 1, Iliffe.

    Google Scholar 

  • Trendelenburg, E. A., Fitton, B., Page, D. E., and Pedersen, A.: 1970 Eldo-Cecles / Esro-Cers Sci. Tech. Rev. 2 1.

    Google Scholar 

  • Tyler, A. F.: 1972, Radio Electr. Eng. 42, 309.

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 1973 D. Reidel Publishing Company, Dordrecht, Holland

About this paper

Cite this paper

Polychronopulos, B., Goodall, C.V. (1973). A System for Measuring and Controlling the Surface Potential of Rockets Flown in the Ionosphere. In: Grard, R.J.L. (eds) Photon and Particle Interactions with Surfaces in Space. Astrophysics and Space Science Library, vol 37. Springer, Dordrecht. https://doi.org/10.1007/978-94-010-2647-5_18

Download citation

  • DOI: https://doi.org/10.1007/978-94-010-2647-5_18

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-94-010-2649-9

  • Online ISBN: 978-94-010-2647-5

  • eBook Packages: Springer Book Archive

Publish with us

Policies and ethics