Solid rocket motors, such as those used on the space shuttle, are composed of a rigid case that contains a thin elastomeric liner and a large area of propellant. This propellant grain consists of an elastomeric material that is highly filled with particulate oxidizer. Magnetic resonance imaging (MRI) has been used to study solid rocket propellants and liner material. The samples studied were simulants, used mainly for safety reasons, of real systems using ammonium sulfate in place of the energetic materials. The polymeric binder was hydroxy-terminated poly(butadiene) (HTPB) reacted with isopherone diisocyanate. MRI was used to observe variations in intensity in the simulant samples due to differing percentages of solids loading. It also showed the homogeneous intensity obtained for an unfilled sample used for comparison with the 82 % filled material. The liner material, HTPB and dimeryl diisocyanate, was imaged despite its relative rigidity observed from its short T2 value. Samples of poly(alkylene) oxide simulants were imaged, and various bubbles and regions of filler inhomogeneity were observed. These defects were correlated with photomicrographs of the sample. MRI can be used to image real systems of solid rocket components.


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    Titel :

    Magnetic resonance imaging study of solid rocket propellants and liners


    Weitere Titelangaben:

    Untersuchung von Feststoffraketentreibstoffen und -ausfütterungen mittels der magnetischen Resonanzabbildung


    Beteiligte:
    Merwin, L.H. (Autor:in) / Nissan, R.A. (Autor:in) / Stephens, T.S. (Autor:in) / Wallner, A.S. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1996


    Format / Umfang :

    8 Seiten, 7 Bilder, 2 Tabellen, 17 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    SOLID ROCKET PROPELLANTS

    Mama, Horrrluz P. | Online Contents | 1996


    Solid Rocket Propellants

    A. I. Silantev | NTIS | 1967


    Solid Rocket Propellants

    A. I. Grigorev | NTIS | 1969


    Environmentally Compatible Solid Rocket Propellants

    Jacox, J. L. / Bradford, D. J. / United States; National Aeronautics and Space Administration | British Library Conference Proceedings | 1995


    Cryogenic Washout of Solid Rocket Propellants

    Elliott, J. P. / Creation, W. P. / Spritzer, M. H. et al. | British Library Conference Proceedings | 1994