Guided missile
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United States of America Patent
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-
Apr 24, 2001
Grant Date -
N/A
app pub date -
Jun 15, 1999
filing date -
Jun 19, 1998
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
A guided missile (12), in particular a projectile which can be fired through a propellent charge gas pressure, having rudder blades (18) which cross each other and which can be pivoted open to steer the missile (12). Each rudder blade (18) is mounted in a guide slot (22) which is closed at the front end by an end portion (26). Each end portion (26) has a spoiler end face (28). Each end portion (26) projects radially beyond the lateral longitudinal ribs (24). At its distal end portion (32) the associated rudder blade (18) is provided with laterally mutually opposite, narrow guide ribs (36) which project out of the rudder blade profile (34).
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