Methods and apparatus for missile air inlet

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

Reexamination Certificate

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Reexamination Certificate

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07851733

ABSTRACT:
Methods and apparatus for delivering a missile may operate in conjunction with a missile comprising an outer skin. The missile may be configured in a closed position and an open position. In the open position, an aperture is opened in the outer skin, for example to supply air to an air-breathing engine. In the closed position, the aperture is closed.

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patent: 3194201 (1965-07-01), Lang
patent: 3414217 (1968-12-01), Kesting
patent: 3495605 (1970-02-01), Gunnarson et al.
patent: 4494459 (1985-01-01), Ziemba
patent: 4526105 (1985-07-01), Herren, Jr.
patent: 6142417 (2000-11-01), Figge, Sr.
patent: 2004/0050056 (2004-03-01), Pederson et al.

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