Thermal protection systems for air and space vehicles having...

Aeronautics and astronautics – Spacecraft – Reusable or returnable

Reexamination Certificate

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Reexamination Certificate

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08056862

ABSTRACT:
A thermal protection system for use upon an air or space vehicle includes a plurality of thermal protection panels formed of a suitable ceramic matrix composition or other thermally protective material each panel having a continuous outer surface free of penetrations or apertures. A plurality of cooperating fasteners are secured between the outer surface of a host vehicle and the undersurface of the thermal protection panels. The fasteners utilize a latching mechanism to secure the panels to the surface of the host air or space vehicle without requiring penetrations or irregularities in the panel surfaces.

REFERENCES:
patent: 3321154 (1967-05-01), Downs
patent: 4012879 (1977-03-01), Aubert et al.
patent: 4804571 (1989-02-01), Jouffreau
patent: 4919366 (1990-04-01), Cormier
patent: 5207544 (1993-05-01), Yamamoto et al.
patent: 5452979 (1995-09-01), Cosenza
patent: 5489074 (1996-02-01), Arnold et al.
patent: 6299106 (2001-10-01), Shorey

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