Mounting arrangement for the pivotally openable rudder blades of a guided missile
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United States of America Patent
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-
Mar 20, 2001
Grant Date -
N/A
app pub date -
Jun 15, 1999
filing date -
Jun 19, 1998
priority date (Note) -
Expired
status (Latency Note)
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Abstract
To maintain control accuracy for the pivotable rudder blades (14), which lie in a combustion chamber, of a guided projectile (12) which can be fired by means of propellent charge, there is provide a mounting arrangement in which the trunnions (20) of the rudder blade holders (16) of the diametrally mutually opposite rudder blades (14) are torsionally stiffly rigidly connected through an associated coupling element (32) which is limitedly resilient in the radial direction of the guided projectile (12).
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