Scram jet engine design

The present invention relates to a scram jet engine for use with a hypersonic vehicle. The scram jet engine has an upper boundary wall, a lower boundary wall, and a plurality of side walls defining an inner air flowpath. The walls are formed by a plurality of tubular heat exchanger panels. Each of t...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: SILLENCE MARK A, NIGAM REVI K, GUINAN DANIEL P, WEBSTER HENRY K, RINELLA SERGIO, SALVADOR COSTANTE, FORTIN THOMAS B, NEMECEK DENNIS J
Format: Patent
Sprache:eng
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