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.
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© 1973 D. Reidel Publishing Company, Dordrecht, Holland
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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
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DOI: https://doi.org/10.1007/978-94-010-2647-5_18
Publisher Name: Springer, Dordrecht
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