|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/322 ; 239/26519 ; 239/26527 ; 239/26529|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 28 인용 특허 : 1|
A steering device comprising an annular element having N exhaust nozzles and a rotary element disposed coaxially inside said annular element; the rotary element comprising M gas passageways may be positioned in MN discrete directions so as to provide a transverse thrust force orientated in one of the steering planes.
A gas jet steering device for a guided missile, said get jet steering device comprising: (a) an annular element having a plurality N of equi-angularly spaced fixed exhaust nozzles inclined at and angle a