Arrangement for thermal protection of an object, such as a therm

Aeronautics and astronautics – Spacecraft – Spacecraft formation – orbit – or interplanetary path

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428920, B64G 158

Patent

active

055117473

ABSTRACT:
Arrangement for the thermal protection of an object, particularly a space vehicle, such as a space missile, including a frame structure covered with thermal insulating material, wherein the material is made of an aggregate of carbon or silica short fibers, the fibers being linked together by means of a binder made of the same constituent and possibly of an appropriate resin. The aggregate is in the form of at least one monobloc element, which is accordingly shaped and dimensioned, and adhered onto the frame structure.

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