Radomes, aircraft and spacecraft including such radomes, and methods of forming radomes

Radomes include an outer wall having a first average thickness and an inner wall having a second average thickness that is different from the first average thickness. At least a major portion of the inner wall is separated from at least a major portion of the outer wall by a space therebetween. The...

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Bibliographische Detailangaben
Hauptverfasser: MACFARLAND ANDREW B, KUHL PAUL C, GLABE JOHN R, JACKSON THOMAS BARRETT
Format: Patent
Sprache:eng
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Zusammenfassung:Radomes include an outer wall having a first average thickness and an inner wall having a second average thickness that is different from the first average thickness. At least a major portion of the inner wall is separated from at least a major portion of the outer wall by a space therebetween. The outer wall may comprise a layer of ceramic matrix composite (CMC) material. Aircraft and spacecraft include such radomes. Methods of forming radomes include forming an outer wall having a first average thickness, forming an inner wall having a different second average thickness, and coupling together the inner wall and the outer wall in such a manner as to provide a space between at least a major portion of the outer wall and at least a major portion of the inner wall.