Title:
ミサイル制御システムおよび方法
Document Type and Number:
Japanese Patent JP4643269
Kind Code:
B2
Abstract:
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.
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Inventors:
Chasman, daniel
Height, Stephen Dee
Fastio, Andrew Bee.
Height, Stephen Dee
Fastio, Andrew Bee.
Application Number:
JP2004551744A
Publication Date:
March 02, 2011
Filing Date:
November 03, 2003
Export Citation:
Assignee:
RAYTHEON COMPANY
International Classes:
F42B10/66; F02K9/80; F42B10/64
Domestic Patent References:
| JP7042615A | ||||
| JP46009927Y1 | ||||
| JP4121600A | ||||
| JP2522167Y2 | ||||
| JP39023494B1 | ||||
| JP7015277B2 | ||||
| JP2548483B2 |
Foreign References:
| FR1217708B1 | ||||
| US3115747 | ||||
| US4432512 |
Attorney, Agent or Firm:
Satoshi Kono
Makoto Nakamura
Kurata Masatoshi
Takashi Mine
Yoshihiro Fukuhara
Sadao Muramatsu
Ryo Hashimoto
Makoto Nakamura
Kurata Masatoshi
Takashi Mine
Yoshihiro Fukuhara
Sadao Muramatsu
Ryo Hashimoto