Fixed canards maneuverability enhancement

A guidance device for projectiles has stationary canards (40) and thrusters (50) positioned on the nose (20) of the projectile (10). The thrusters (50) are initiated from remote or local sensor to provide flight maneuverability to a target.

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Bibliographische Detailangaben
Hauptverfasser: FARINA ANTHONY, TOLEDO WILFREDO, AMORUSO MICHAEL J
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A guidance device for projectiles has stationary canards (40) and thrusters (50) positioned on the nose (20) of the projectile (10). The thrusters (50) are initiated from remote or local sensor to provide flight maneuverability to a target.