This presentation focuses on the effects of the space environment on spacecraft systems and applying this knowledge to spacecraft pre-launch engineering and operations. Particle radiation, neutral gas particles, ultraviolet and x-rays, as well as micrometeoroids and orbital debris in the space environment have various effects on spacecraft systems, including degradation of microelectronic and optical components, physical damage, orbital decay, biasing of instrument readings, and system shutdowns. Space climate and weather must be considered during the mission life cycle (mission concept, mission planning, systems design, and launch and operations) to minimize and manage risk to both the spacecraft and its systems. A space environment model for use in the mission life cycle is presented.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Application of Space Environmental Observations to Spacecraft Pre-Launch Engineering and Spacecraft Operations


    Beteiligte:
    J. L. Barth (Autor:in) / M. Xapsos (Autor:in)

    Erscheinungsdatum :

    2008


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Spacecraft Processing and Launch Operations

    Parrish, Mike / Koby, Kenneth | AIAA | 2021


    SPACECRAFT LAUNCH SYSTEM AND LAUNCH METHOD, AND SPACECRAFT

    ZHANG ZHIGANG | Europäisches Patentamt | 2022

    Freier Zugriff


    SPACECRAFT LAUNCH UNIT

    STOROZH ALEKSANDR DMITRIEVICH / LUKASHCHUK IVAN PETROVICH / SHAPARENKO PAVEL YUREVICH et al. | Europäisches Patentamt | 2020

    Freier Zugriff