Title:
空気力学的弾頭冠により保護された誘導兵器
Document Type and Number:
Japanese Patent JP2013530367
Kind Code:
A
Abstract:
In the field of steered munitions intended to destroy a target after at least one flight phase followed by a target approach phase, a munition comprises a munition body of cylindrical shape of longitudinal axis having, on the same side as a front end of the munition which is the end intended to be directed toward the target, a front body comprising an optic of a guidance device that guides said munition toward the target, a cap for protecting the optic, secured to the munition body, characterized in that the protective cap comprises at least one recess having a pyrotechnic device intended to destroy said protective cap so as to free the optic and make the munition guidance device operational during the target approach phase. Application: steered or guided munitions such as those of the rocket or projectile type, or missiles.
Inventors:
Coe, patrick
Morrow, Fabian
Morrow, Fabian
Application Number:
JP2013509566A
Publication Date:
July 25, 2013
Filing Date:
May 11, 2011
Export Citation:
Assignee:
Tedea Amemon SAS
International Classes:
F42B10/46
Attorney, Agent or Firm:
Takahisa Kimura