|국가/구분||United States(US) Patent 등록|
|우선권정보||DE-102 05 043(2002-02-07)|
|§371/§102 date||20040809 (20040809)|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 10 인용 특허 : 9|
A missile to be fired from a barrel contains a tail, a tail sleeve attached to the tail, a stop element fixed to the tail sleeve, and a movable structural part disposed at the tail. Fin assembly wings are provided and are to be released from a subcaliber launch position to an overcaliber functional position by the movable structural part moving toward the stop element through a given distance. A pressure area is disposed between the tail end surface and the movable structural part. A propellant gas enters the pressure area during the firing of the missil...
What is claimed is: 1. A missile to be fired from a barrel, comprising: a tail having a tail end surface; a tail sleeve attached to said tail; a stop element fixed to said tail sleeve; a movable structural part disposed at said tail; fin assembly wings to be released from a subcaliber launch position to an overcaliber functional position by said movable structural part moving toward said stop element through a given distance, said fin assembly wings having cutouts formed therein; a pressure area disposed between said tail end surface and said movable s...