AbstractTotally 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 find 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 cylinrical 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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    Titel :

    Electrodynamics payloads for small rockets


    Beteiligte:
    Croskey, C.L. (Autor:in) / Hale, L.C. (Autor:in) / Mitchell, J.D. (Autor:in) / McCarthy, S.P. (Autor:in) / Goodnow, K.J. (Autor:in) / Li, C. (Autor:in) / Goldberg, R.A. (Autor:in)

    Erschienen in:

    Advances in Space Research ; 12 , 10 ; 321-324


    Erscheinungsdatum :

    1992-01-01


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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