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NASA NTRS · 19920061697

Electrodynamics payloads for small rockets

Abstract

Totally integrated design facilitates electrical cleanliness and light weight, which are necessary in subsonic parachute-borne payloads for electrodynamics investigations. 'Blunt' probes measure ion conductivity, as do Gerdien condensers. Recent finite-element computer analyses combining flow and electrodynamics have resolved problems in determining ion densities and mobilities from Gerdien data. Three-axis electric fields are measured with deployable boom-mounted electrodes from dc through VLF. Splitting the cylindrical payload with an insulator and measuring the current between halves has provided a vertical Maxwell current detector mechanically rigid enough to measure, at ELF, energy related to coupling. A nose tip 'Smith' probe turbulence measurement is usually performed on ascent. Other instrumentation, such as photo-ionization sources and X-ray detectors, can also be included. These electrodynamic measurement payloads are about one meter in length and have a mass of about 9 kg. They can be launched with an Orion-class or smaller vehicle.

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BibTeXRIS

Croskey, C. L., Hale, L. C., Mitchell, J. D., Mccarthy, S. P., Goodnow, K. J., Li, C., Goldberg, R. A.. 1992-10-01. Electrodynamics payloads for small rockets. https://ntrs.nasa.gov/citations/19920061697

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