It is shown that first generation of space simulators provides capability for testing components and their functioning in routine fashion up to 700-km orbit altitudes; second generation provides simulation of solar thermal effects and reliability testing of propulsion and mission support mechanisms in lower orbit levels up to 700 km; concepts under study point to third generation which may make it possible to develop ideal space chamber, capable of simulating celestial radiation, absorbing reflected and reradiated heat, and establishing molecular sink for rejected gases.


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    Titel :

    Simulating interplanetary space


    Weitere Titelangaben:

    Astronautics Aerospace Eng


    Beteiligte:
    Hnilicka, M.P. (Autor:in) / Geiger, K.A. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Conquering interplanetary space

    Peschka, W. | Engineering Index Backfile | 1956


    Propulsion for interplanetary space missions

    Kirby, F.M. | Engineering Index Backfile | 1962


    Thermal Environment of Interplanetary Space

    Christensen, E. H. / Ballinger, J. C. / Elizalde, J. C. | SAE Technical Papers | 1962


    Pollution potentials in interplanetary space

    Keay, C. S. L. / International Council of Scientific Union; Committee on Space Research | British Library Conference Proceedings | 1998