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.
