FULL-CALIBER, SPIN-STABILIZED GUIDED PROJECTILE WITH LONG RANGE
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United States of America Patent
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Issued Date -
Apr 27, 2017
app pub date -
Oct 26, 2016
filing date -
Oct 27, 2015
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Abstract
An increased range guided projectile includes overcaliber lateral moment reducing wings (10) that can be deployed. The lateral moment reducing wings (10) are designed and arranged behind the center of gravity (S) in the tail direction on the guided projectile (1) so that the pitching moment derivative coefficient (Cmα) of the guided projectile (1) is in the range of ±0.5, if the guided projectile (1) has a speed that is in the speed range of Mach 0.4 to 0.8; the lateral moment reducing wings (10) are in their deployed position; and, the canard guide device (20) does not exert any guiding moments.
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