Finlet injector

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

Patent

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Details

244 322, 244117A, B64C 2108

Patent

active

042202973

ABSTRACT:
A finlet injector for external burning fuel injection is provided to obtain a higher performance through a combination of more optimum air-to-fuel ratio and better air/fuel mixing. This is done by capturing (mixing with) a greater quantity of air for a given fuel injection pressure and flow rate. The device is thermally protected and for most flight regimes has minimum drag.

REFERENCES:
patent: 3682100 (1972-08-01), Lundberg, Jr.
patent: 3745928 (1973-07-01), Kinnaird et al.
patent: 3770226 (1973-11-01), Kranz
patent: 4151800 (1979-05-01), Dotts et al.
Asymmetric "Penshape" Nozzles in Jet Carnard Configurations for Attitude trol by Robert W. Cubbison NASA Tech. Note D 1561.

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