In FY 2002 a team of engineers and scientists at MSFC conducted a preliminary investigation of the options for deflecting a Near Earth Object (NEO) fiom a collision course with the earth. A general discussion of the current threat facing the earth from NEO s is outlined. A suite of tools were developed to model inbound and outbound trajectories, propulsive options, and assessment of threat. Propulsive options considered included; staged chemical, nuclear ablation and deflagration, mass driver and solar sail concepts. Trajectory tools plotted the outbound course to intercept the NE0 and the deflection requirements to cause the inbound NE0 to miss the earth. Threat assessment tools estimated the number of lives saved over a given time frame by deploying a system capable of deflecting an NE0 of a certain size and velocity. All of these tools were integrated into a routine to find the most effective vehicle for a given mission mass and mission time. Discussion of desired future efforts is given. This work was funded under the Revolutionary Aerospace Systems Concepts activity from NASA HQ.


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    Titel :

    Planetary Defense: Options for Deflection of Near Earth Objects


    Beteiligte:
    Adams, Robert B. (Autor:in) / Alexander, Reginald (Autor:in) / Bonometti, Joseph (Autor:in) / Chapman, Jack (Autor:in) / Fincher, Sharon (Autor:in) / Hopkins, Randall (Autor:in) / Kalkstein, Matthew (Autor:in) / Philips, Al (Autor:in) / Polsgrove, Tara (Autor:in) / Statham, Geoffrey (Autor:in)

    Kongress:

    Joint Propulsion Conference ; 2003 ; Huntsville, AL, United States


    Erscheinungsdatum :

    01.01.2002


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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