|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F42B-010/66 F42B-010/00 F02K-009/80 F02K-009/00|
|미국특허분류(USC)||244/003.22; 244/003.1; 244/003.15; 244/003.21|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 4 인용 특허 : 15|
A missile includes a tail section having a multi-nozzle grid with both fixed nozzlettes, and movable, thrust vector nozzlettes. The movable nozzlettes may be configured in a number of discrete array bars, each containing multiple of the movable nozzlettes. Movement of one or more array bars may be used to vector the thrust of the missile, providing roll, yaw, or spinning of the missile, for example.
What is claimed is: 1. A missile comprising: a nozzle grid including: a plurality of fixed nozzles; and a plurality of movable nozzles; and a pressurized gas source operatively coupled to the nozzle grid; wherein the movable nozzles are divided up into plural separately-actuatable arrays; and wherein the movable nozzles of each of the arrays are in a separate array bar. 2. The missile of claim 1, wherein the missile includes four array bars. 3. The missile of claim 1, wherein the array bars are axisymmetrically spaced about an axis of the mi...