RIGIDIZED HYBRID INSULATING NON-OXIDE THERMAL PROTECTION SYSTEM AND METHOD OF PRODUCING A NON-OXIDE CERAMIC COMPOSITE FOR MAKING THE SAME

A thermal protection system (200) is provided for a vehicle substructure. The thermal protection system (200) comprises an outer layer (210) for protecting the vehicle substructure. The thermal protection system (200) further comprises an inner layer (220) for conforming to the vehicle substructure...

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Bibliographische Detailangaben
Hauptverfasser:	DRIEMEYER, Dan E, PINNEY, Thomas R, MOBERS, Patrick J, CHEN, Winnie W, EMBLER, Jonathan D, HENG, Vann, SALAMA, Merna E, LEHMAN, Leanne L
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARTIFICIAL STONE AVIATION CEMENTS CERAMICS CHEMISTRY COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDINGMATERIALS CONCRETE COSMONAUTICS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM LIME, MAGNESIA METALLURGY PERFORMING OPERATIONS REFRACTORIES SLAG TRANSPORTING TREATMENT OF NATURAL STONE VEHICLES OR EQUIPMENT THEREFOR
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Beschreibung
Zusammenfassung:	A thermal protection system (200) is provided for a vehicle substructure. The thermal protection system (200) comprises an outer layer (210) for protecting the vehicle substructure. The thermal protection system (200) further comprises an inner layer (220) for conforming to the vehicle substructure (108). The thermal protection system (200) also comprises an insulation layer (230) sandwiched between the inner and outer layers (210,220). The insulation layer (230) includes a porous low-density ceramic insulating material having a densified portion (232) that covers an inner surface of the outer layer (210) to strengthen adhesion.