The feasibility of a solar sonde mission with a 0.26 AU perihelion was investigated. The scientific useful load, thrust requirements, construction, and possible carrier rockets are discussed along with earth-sun orbits, and design criteria. It is concluded that there is a high degree of probability of success for the solar sonde, and for launching, the Saturn 5 carrier rocket can be used.


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    Titel :

    Study of a Solar Sonde in the Ecliptic with an Approach to the Sun to within 0.26 au


    Beteiligte:
    D. E. Koelle (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    201 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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    C. A. Price / T. G. Chambers | NTIS | 1976


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    Solar out-of-Ecliptic Study. Volume 1: Executive Summary

    T. G. Chambers / E. P. L. Windsor | NTIS | 1976


    Solar out-of-Ecliptic Study. Volume 2: System Analysis and Definition

    T. G. Chambers / E. P. L. Windsor | NTIS | 1976