Description Over the past 25 years, the mass of man-made objects from upper-stage breakups has grown to the point that it now dictates the design environment for future low-Earth-orbit operations. The hazards presented by a vast range of particle sizes, from virtual dust to the largest known orbital debris fragments, have not been fully quantified, but the field struggles with that task now. This book provides an overview of the problem, discusses practical strategies for mitigation of debris hazards, and considers strategies for prevention of future breakups.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Explosive Fragmentation of Orbiting Propellant Tanks


    Contributors:


    Publication date :

    1989-01-01




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English



    Explosive fragmentation of orbiting propellant tanks

    Benz, F. J. / Kays, R. L. / Bishop, C. V. et al. | NTRS | 1989


    Propellant resupply of orbiting spacecraft

    Bloznalis, P. J. / Lupien, R. / Sudbay, M. et al. | NTRS | 1989




    Composite reinforced propellant tanks

    Brown, L. D. / Martin, M. J. / Aleck, B. J. et al. | NTRS | 1975