Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1986-09-05
1988-02-23
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F42B 15033
Patent
active
047265442
ABSTRACT:
A steering block for the final phase of a guided projectile comprises control jets acted upon by hot gas created in a combustion chamber. A preferred embodiment of more compact and acceleration resistant construction, uses four control jets arranged lying in the cross sectional plane of the projectile casing equidistantly distributed around the circumference of the projectile casing. Each control jet has a corresponding valve likewise arranged lying in a plane in such a way that their longitudinal axes extend along chords of the circular cross section of the projectile casing. In another preferred embodiment, for purposes of further cost reduction in volume and weight, the valves have an adjusting member made of memory alloy which is electrothermically acted upon by way of a heating element.
REFERENCES:
patent: 3139725 (1964-07-01), Webb
patent: 3807660 (1974-04-01), LeCorviger et al.
patent: 4541592 (1985-09-01), Moll
Baumgart; Krupp Technical Communication, No. 1, 1976.
Mueller; "Natural Sciences", 1984, pp. 507, 512, & 514.
Schetky; "Spectrum of Nature" 1980; pp. 48, 49, & 57.
Innovative Technology International, Inc. publication.
Jordan Charles T.
Rheinmetall GmbH
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