Rocket motor insulation

Stock material or miscellaneous articles – Web or sheet containing structurally defined element or... – Including a second component containing structurally defined...

Reexamination Certificate

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Details

C264S497000, C425S174400, C425S375000

Reexamination Certificate

active

07820285

ABSTRACT:
Provided is a solid rocket motor (SRM) insulation, wherein carbon nano fibers (CNF) are blended into a polyurethane matrix so as to disperse the CNF in the polymer. The so blended material is then extruded, injection molded or sprayed on or into the desired shape. Such SRM insulation has reduced ablation over prior art insulations, resulting in reduction in weight of the insulation needed in such rockets, permitting increase of payload therein.

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patent: 5603170 (1997-02-01), Hirai
patent: 6680016 (2004-01-01), Wang et al.
patent: 6691505 (2004-02-01), Harvey et al.
patent: 7045088 (2006-05-01), Matsumiya et al.
patent: 7494946 (2009-02-01), Gibson et al.
patent: 2002/0018847 (2002-02-01), Guillot
patent: 2002/0137871 (2002-09-01), Wheeler et al.
patent: 2007/0290410 (2007-12-01), Koo et al.

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