|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F41G-007/00 F42B-010/60 F42B-015/01|
|미국특허분류(USC)||244/315 ; 244/322|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 34 인용 특허 : 0|
A guided projectile, especially a propelled or ballistic missile, has its trajectory corrected by gas jets from pulse thrusters disposed in at least on axial plane of the missile symmetrically on opposite sides of the center of gravity thereof and whose thrusts are countered, when no longer needed, by the operation of diametrically opposite pulse thrusters in the same plane and at the same side of the center of gravity. The pulse thrusters are formed as gas generators which can be triggered to feed respective nozzles. The projectile is also roll stabiliz...
A guided projectile comprising: an elongated axially extending projectile body having a front end, a rear end and a center of gravity located along the axis of said body between said ends; a plurality of pulse thrusters axially spaced along said body and each provided with a pair of diametrically opposite, oppositely opening thrust nozzles lying in a guidance director plane, the nozzles of both said pulse thrusters being disposed symmetrically on opposite sides of said center of gravity in the same guidance director plane; respective triggerable-release ...