|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 20 인용 특허 : 1|
A steering arrangement for missile type projectiles. A source of steering propulsion which is accommodated in the vicinity of the center of gravity of the missile comprises two gas generators which are positioned symmetrically on either side of the center of gravity a system being provided to switch or divert the gases to the exterior of the missile in at least two directions which are transverse to the projectile and to its axis. The arrangement according to the invention considerably improves the reliability and effectiveness with which the projectile ...
A piloting arrangement for a guided missile having a body comprising, in combination, two gas generators in said missile body for providing a source of gas flow, said two gas generators being coupled in parallel and disposed symmetrically at either side of the center of gravity of said missile body, a nozzle having a throat disposed between said two gas generators coaxially with the longitudinal axis of said missile, conduit means in said missile for conducting said gas flow from said gas generators to said nozzle throat, a plurality of peripheral ejecti...