The development of new instrumentation and associated data reduction programs for measuring the orientation attitude of spin-stabilized sounding rockets or satellites has provided a simple low-cost system that is accurate to within 2 deg. The instrumentation has been successfully flown in one satellite and in more than 20 sounding rockets. This paper describes the system performance obtained on two of the sounding rocket flights. (Author)


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    Titel :

    Space Vehicle Attitude Studies


    Beteiligte:
    C. D. Howard (Autor:in) / D. J. Innes (Autor:in) / D. Mansir (Autor:in)

    Erscheinungsdatum :

    1968


    Format / Umfang :

    27 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Doolin, B.F. | Engineering Index Backfile | 1962


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