专利内容由知识产权出版社提供
专利名称：ROCKET ENGINE SYSTEMS WITH AN
INDEPENDENTLY REGULATED COOLINGSYSTEM
发明人：PATRICK R.E. BAHN,EARL W. RENAUD申请号：US157865申请日：20171017
公开号：US20180238271A1公开日：20180823
专利附图：
摘要：An improved rocket engine system including a rocket engine, a coolant source,and a propellant source. Each of coolant source and propellant source is in operative
communication with rocket engine whereby there is independent regulation or control ofcoolant source flow relative to propellant source flow. The improved rocket enginesystem may further include one or more of: at least one power source, at least onepower source motor, at least one pump, at least one controller, and a propellantpressurizing source. The propellant source preferably includes a fuel source and anoxidizer source. An embodiment includes a cooling system with a coolant source, a fuelsystem with a fuel source, an oxidizer system with an oxidizer source, a propellantpressurizing system with a propellant pressurizing source, multiple pumps, an assemblyof power source and controller, and a main rocket engine assembly.
申请人：PATRICK R.E. BAHN,EARL W. RENAUD
地址：WASHINGTON DC US,OTTAWA CA
国籍：US,CA
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