ROCKET NOZZLE THROAT INSERT

A rocket throat insert including an annular body having a radially inner annular wall portion and a radially outer annular portion. The inner wall portion has a contoured radially inner surface defining a nozzle throat. The outer portion includes an annular buttressing structure supporting the inner...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: FOWLER, Gray, BRENNAN, Michael
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:A rocket throat insert including an annular body having a radially inner annular wall portion and a radially outer annular portion. The inner wall portion has a contoured radially inner surface defining a nozzle throat. The outer portion includes an annular buttressing structure supporting the inner wall portion and defining one or more insulation gaps arranged annularly around the inner wall portion. The insulation gaps restrict the radial flow of heat through the annular body.