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Artikel-Nr. 17202426


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Autor(en): 
  • Heiner Klinkrad
  • Space Debris: Models and Risk Analysis 
     

    (Buch)
    Dieser Artikel gilt, aufgrund seiner Grösse, beim Versand als 3 Artikel!


    Übersicht

    Auf mobile öffnen
     
    Lieferstatus:   Auf Bestellung (Lieferzeit unbekannt)
    Veröffentlichung:  November 2014  
    Genre:  Naturwissensch., Medizin, Technik 
     
    Aerospace engineering / Aerospace Technology and Astronautics / astronautics / Automotive (motor mechanic) skills / Automotive Engineering / Automotive technology & trades / B / engineering / environment;modeling;risk;risk analysis;space;traffic / Industrial and Production Engineering / Industrial safety / Probability & statistics / quality control / Quality Control, Reliability, Safety and Risk / reliability / Reliability engineering / Space Physics / Space sciences / Statistics
    ISBN:  9783642426230 
    EAN-Code: 
    9783642426230 
    Verlag:  Springer Nature EN 
    Einband:  Kartoniert  
    Sprache:  English  
    Serie:  Astronautical Engineering
    Springer Praxis Books  
    Dimensionen:  H 244 mm / B 170 mm / D  
    Gewicht:  757 gr 
    Seiten:  430 
    Zus. Info:  Previously published in hardcover 
    Bewertung: Titel bewerten / Meinung schreiben
    Inhalt:
    In Space Debris Models and Risk Analysis the authors will provide the reader with a comprehensive background to understand the various sources of space debris, and to assess associated risks due to the current and future space debris environment. Apart from the non-trackable objects produced by historic on-orbit fragmentation events, several other sources of space debris will be outlined. Models will be described to allow the generation and propagation of the different debris families and permit the assessment of the associated collision risk on representative target orbits for present and future conditions. Using traffic models and possible mitigation practices, the future evolution of the space debris environment will be forecast. For large-size, trackable objects methods will be described for conjunction event predictions and related risk assessments. For hazardous re-entry objects, procedures will be outlined to enable the prediction of re-entry times and likely impact areas, to assess uncertainties in these factors, and to quantify the risk due to ground impact. Models will also be described for meteoroids, which prevail over space debris at small particle sizes.

      
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