Decoy missile

Details Decoy missile Decoy missile

1966-02-15

1982-07-20

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Remote control

244158R, 244160, B64G 100

Patent

active

043401970

ABSTRACT:
A decoy missile having a high moment of inertia with a corresponding reduction of the natural oscillation frequency for simulating reentry of a ballistic nose cone into the earth's atmosphere. High density ballast material disposed in the forward section is in proportional relationship to similar ballast material in the base section such that the distance between the center of pressure and the center of gravity is equal to one-half the base diameter.

REFERENCES:
patent: 603466 (1898-05-01), Hammer
patent: 2957417 (1960-10-01), Musgrave
patent: 3200747 (1965-08-01), Sorenson et al.
patent: 3270503 (1966-09-01), Meyer, Jr.
patent: 3290681 (1966-12-01), Beteille

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