Dual Manifold High Performance Throttleable Injector.
DEPARTMENT OF THE AIR FORCE WASHINGTON D C
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This patent describes a dual manifold propellent injector having at least four distinct platelets in its configuration. The first two platelets constituting the primary and secondary fuel platelets the third and fourth platelets constituting the primary and secondary oxidizer platelets. By proper valve throttling, the injector is capable of providing homogeneous, intimately mixed propellants at all thrust levels. Author
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