Inflatable missle airframe surfaces

Details Inflatable missle airframe surfaces Inflatable missle airframe surfaces

1986-06-16

1988-09-13

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Remote control

102293, F42B 1502

Patent

active

047703695

ABSTRACT:
This invention relates to an inflatable aerodynamic surface (14) particularly adapted for improving the aerodynamic smoothness of the forward end of a missile (10) of the type having a relatively blunt forward end with a centrally disposed extendible probe member (26). In accordance with this invention, a flexible membrane (36) is provided having a base edge (46) sealingly affixed to the forward edge of the missile casing and an apex (48) affixed to the forward end of the probe (26). The membrane (36) is inflated by a gas generator (42) to pressurize the inside of the membrane to define a smooth, nose-shaped aerodynamic frontal surface.

REFERENCES:
patent: 2377839 (1945-06-01), Dake
patent: 3053488 (1962-09-01), Cox
patent: 3086467 (1963-04-01), Gallagher et al.
patent: 3710716 (1973-01-01), Davis et al.
patent: 4166597 (1979-09-01), Seifert et al.
patent: 4181079 (1980-01-01), Klier et al.
patent: 4549464 (1985-10-01), Hawkins et al.

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