Granted Patent
Utility
US 6,209,199 · App. 09/271,394
Method of manufacturing a high heat flux regenerative circuit, in particular for the combustion chamber of a rocket engine
Inventors:
Daniel Cornu, Christophe Verdy, Jean-Michel De Monicault, Christian Coddet
Patented Case
View Patent ↗
Granted: Apr 3, 2001
Filed: Mar 17, 1999
Inventors
Daniel Cornu
Christophe Verdy
Jean-Michel De Monicault
Christian Coddet
Assignee (at issue)
Societe Nationale d'Etude et de Construction de Moteurs d'Aviation - S.N.E.C.M.A
This patent predates the USPTO's electronic file wrapper — prosecution documents from this era exist only in the Patent Office's paper records. A certified copy of the file history can be ordered from the USPTO's paper archives.