Supersonic projectile nose cones with flat tips are disclosed. An example apparatus includes a nose cone for a projectile configured for supersonic flight at velocities of at least Mach 2.0. The nose cone has an axisymmetric body extending from a base to a tip. The body has a thickness and defines an interior cavity. The tip is defined by a flat face normal to a central axis of the projectile.
SUPERSONIC PROJECTILE NOSE CONES WITH FLAT TIPS
2016-09-01
Patent
Elektronische Ressource
Englisch
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