Invention Grant
- Patent Title: Micro-coaxial injector for rocket engine
- Patent Title (中): 微型同轴喷油器用于火箭发动机
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Application No.: US11752866Application Date: 2007-05-23
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Publication No.: US07900435B1Publication Date: 2011-03-08
- Inventor: Jeffrey K. Greason , Douglas B. Jones , Daniel L. DeLong
- Applicant: Jeffrey K. Greason , Douglas B. Jones , Daniel L. DeLong
- Applicant Address: US CA Mojave
- Assignee: XCOR Aerospace
- Current Assignee: XCOR Aerospace
- Current Assignee Address: US CA Mojave
- Agency: McDermott Will & Emery LLP
- Main IPC: F02K9/00
- IPC: F02K9/00

Abstract:
An improved coaxial injector for injecting first and second propellants into a combustion chamber of a rocket engine is provided. The injector includes a first plate, a second plate, a plurality of channels formed in the first plate, and a plurality of tubes extending through the second plate and into the plurality of channels. The tubes inject a first propellant, such as an oxidizer, into the combustion chamber, and the channels inject a second propellant, such as a fuel, around the tubes and into the combustion chamber.
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