Thrust vector control by circulation control over aerodynamic su

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle – With addition of secondary fluid upstream of outlet

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60231, 23926523, 244207, 244 52, B64C 1510

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active

040636852

ABSTRACT:
Aerodynamic surfaces are fixedly mounted in the diverging section of a rot nozzle and a fluid is injected through the fixed jet vane to flow about the vane. Fluid flow is controlled to make it appear that from upstream the jet vane is at an angle of attack. This deflects the main flow and produces side force. A minimum of injection flow enables high side forces to be obtained for missile control.

REFERENCES:
patent: 2943821 (1960-07-01), Wetherbee, Jr.
patent: 3221498 (1965-12-01), Bankston
patent: 3229460 (1966-01-01), Jones
patent: 3325103 (1967-06-01), Abbott
patent: 3350886 (1967-11-01), Feraud et al.
patent: 3435837 (1969-04-01), Sher

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