Re-entry of space hardware into the atmosphere is a recommended technique for disposal of space hardware at end of life. However, while aerodynamic heating and loads will break a reentering object apart and a substantial fraction of the object's mass will be melted away, evidence shows that large and potentially hazardous fragments can survive re-entry and impact the Earth's surface. Standards and regulations are emerging that will limit the acceptable hazard and require that space hardware exceeding a survivability threshold be deorbited into a safe ocean area. The current paper provides an overview of re-entry breakup, presents on-the-ground evidence that large, hazardous objects survive, highlights current guidelines, and requirements to limit the hazard to people and property, and discusses how re-entry hazards are estimated.


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    Titel :

    Spacecraft re-entry strategies: Meeting debris mitigation and ground safety requirements


    Beteiligte:
    Ailor, W H (Autor:in) / Patera, R P (Autor:in)


    Erscheinungsdatum :

    01.06.2007


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch