Missile head and method for separating a shroud from a fuselage of a missile
AssigneeDiehl Bgt Defence GmbH & Co. KG
InventorsPeter Gerd Fisch, Dirk Bross, Dominik Herrmann, Peter Mangold
Life of this patent
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AssigneeDiehl Bgt Defence GmbH & Co. KG
InventorsPeter Gerd Fisch, Dirk Bross, Dominik Herrmann, Peter Mangold
Estimating the term…
A missile head has a shroud which forms its tip and which can be detached in its totality during flight from the fuselage of the missile. The missile head further has a rear part, which is connected to the fuselage, and a front nose, which can be disconnected from the rear part and forms the tip. A separating device separates the rear part from the fuselage and the nose from the rear part during flight. A physically small shroud can be achieved, and damage to the fuselage of the missile by separation of the shroud can be prevented, if the nose is split into at least two parts and the separating device is prepared to split the nose into these two parts during flight.
A missile head of a missile, comprising:
A method of separating a shroud from a fuselage of a missile during flight of the missile, the method which comprises:
A method of separating a shroud from a fuselage of a missile during flight of the missile, the method which comprises:
Dependencies are inferred from the claim text.