|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F42B-012/56 F42B-015/10 F42B-012/46 F42C-014/00 F42B-012/02 F42B-010/02 F42B-010/30|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 57|
A rocket-propelled grenade includes a payload section, a selectable fuzing section joined to the payload section, and a propulsion section joined to the selectable fuzing section. A rocket-propelled grenade includes a propulsion section and a payload section operably associated with the propulsion section. The payload section includes a shell, one or more penetrators disposed in the shell, and a charge for compromising the shell to deploy the one or more penetrators when the charge is initiated.
1. A rocket-propelled grenade, comprising: a propulsion section comprising a booster propellant housing defining a nozzle and a groove;a payload section operably associated with the propulsion section and joined to the booster propellant housing, the payload section comprising: a shell;one or more penetrators disposed in the shell; anda charge for compromising the shell to deploy the one or more penetrators when the charge is initiated;a plurality of fins operably associated with the booster propellant housing;a plurality of biasing elements, correspondi...