METHOD FOR MANUFACTURING COMBUSTOR OF ROCKET ENGINE, COMBUSTOR OF ROCKET ENGINE, AND ROCKET ENGINE

In the present invention, a method for manufacturing a combustor of a rocket engine comprises: a step for preparing a combustor inner tube (20) having a cooling groove (24); a step for providing an outer layer (30) on an outer circumferential surface of the combustor inner tube (20) so as to cover t...

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Bibliographische Detailangaben
Hauptverfasser: TAKAHASHI TAKAYUKI, KAJIMA KAZUHIRO, TSUZUKI TAMAKI
Format: Patent
Sprache:eng ; fre ; jpn
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