APPARATUS FOR DESUPERHEATING HIGH TEMPERATURE, HIGH VELOCITY STEAM

A desuperheating spray chamber for use in a rocket exhaust recovery system for a nuclear thermal propulsion rocket, including a substantially-cylindrical outer tank with an upper end including an entrance port and two exhaust ports, a substantially-cylindrical shroud extending downwardly from an inn...

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Bibliographische Detailangaben
Hauptverfasser: Inman, James Brian, Ziegler, Ryan Z, Gustafson, Jeremy Leslie, Fisher, Charles Larry, Martin, Robert Paul
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A desuperheating spray chamber for use in a rocket exhaust recovery system for a nuclear thermal propulsion rocket, including a substantially-cylindrical outer tank with an upper end including an entrance port and two exhaust ports, a substantially-cylindrical shroud extending downwardly from an inner surface of the upper end of the tank, an annular inner spray ring that is both disposed within and concentric with the shroud; and an annular outer spray ring that is disposed between a side wall of the outer tank and the shroud, the annular outer ring being concentric with the shroud.