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US 2015/0027102 A1Published application
Tri-propellant rocket engine for space launch applications
OwnerPatrick R.E. Bahn, Earl W. Renaudinventors
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Abstract
A tri-propellant rocket engine for space launch applications is disclosed. The tri-propellant rocket engine comprises three main assemblies: an injector, a chamber head, and a chamber.
Claims7
A tri-propellant rocket engine for space launch applications comprising:
- an injector;
- whereis said injector is an independent dual sleeve pintle injector that allows the independent control of velocity vector, momentum vector, liquid propellant pressure, propellant volument and vorticity;
- a chamber head, wherein said chamber head serves as a mechanical support for said pintle injector and propellant injection manifolds;
- and a chamber.
1 more element
Dependencies are inferred from the claim text.