The New Horizons (NH) spacecraft was launched in January 2006 aboard an Atlas V launch vehicle, in a mission to explore Pluto, its moons, and other bodies in the Kuiper Belt. The NH spacecraft is powered by a Radioisotope Thermoelectric Generator (RTG) which encases multiple General Purpose Heat Source (GPHS) modules. Thus, a pre-launch vehicle breakup analysis for an inadvertent atmospheric reentry in the event of a launch failure was required to assess aerospace nuclear safety and for launch contingency planning. This paper addresses potential accidental Earth reentries analyzed at the Jet Propulsion Laboratory (JPL) which may arise during the ascent to parking orbit, resulting in a suborbital reentry, as well as a departure from parking orbit, resulting in an orbital reentry.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Inadvertent Earth Reentry Breakup Analysis for the New Horizons Mission


    Beteiligte:
    Ling, Lisa M. (Autor:in) / Salama, Ahmed (Autor:in) / Ivanov, Mark (Autor:in) / McRonald, Angus (Autor:in)

    Kongress:

    2nd IAASS Confeence Space Safety in a GLobal World ; 2007 ; Netherlands


    Erscheinungsdatum :

    2007-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    INADVERTENT EARTH REENTRY BREAKUP ANALYSIS FOR THE NEW HORIZONS MISSION

    Ling, L. / Salama, A. / Ivanov, M. et al. | British Library Conference Proceedings | 2007


    Analysis of the Inadvertent Reentry of the Cassini Spacecraft's Radioisotope Thermoelectric Generators

    Daywitt, J. E. / Bhutta, B. A. / Vacek, D. J. et al. | British Library Conference Proceedings | 1999


    Analysis of the Inadvertent Reentry of the Cassini Spacecraft's Radioisotope Thermoelectric Generators

    Frank, M. V. / Ailor, W. H. / University of New Mexico; School of Engineering; Institute for Space and Nuclear Power Studies | British Library Conference Proceedings | 1999


    REENTRY HEATING AND THERMAL PROTECTION OF A MARS-MISSION EARTH-REENTRY MODULE

    CHIN, J.H. / HEARNE, L.F. / LEFFERDO, J.M. | AIAA | 1964


    REENTRY BREAKUP RECORDER: CONCEPT, TESTING, MOVING FORWARD

    Weaver, M.A. / Ailor, W.H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012