Methods and apparatus for increasing aerodynamic performance of projectiles
First Claim
1. An unmanned projectile, the projectile comprising at least one of the following enhancements to increase its aerodynamic performance:
- means for deploying at least one wing from a body of the projectile after launch thereof; and
means for deploying a fin from the body of the projectile after launch thereof.
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Abstract
A method for enhancing an aerodynamic performance of an unmanned projectile. The method including at least one of the following: (a) morphing a cross-sectional shape of the projectile after launch thereof; (b) morphing a longitudinal shape of the projectile after launch thereof; (c) bleeding a fluid at a base of the projectile during flight thereof: (d) varying a base cone angle of the projectile as a function of speed thereof; (e) deploying at least one wing from a body of the projectile after launch thereof; and (f) deploying a fin from the body of the projectile after launch thereof.
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Citations
28 Claims
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1. An unmanned projectile, the projectile comprising at least one of the following enhancements to increase its aerodynamic performance:
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means for deploying at least one wing from a body of the projectile after launch thereof; and
means for deploying a fin from the body of the projectile after launch thereof. - View Dependent Claims (14, 15, 16, 17, 18, 19)
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2-13. -13. (canceled)
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20. A method for enhancing an aerodynamic performance of an unmanned projectile, the method comprising at least one of the following:
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deploying at least one wing from a body of the projectile after launch thereof; and
deploying a fin from the body of the projectile after launch thereof. - View Dependent Claims (25, 26, 27, 28)
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21-24. -24. (canceled)
Specification