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Methods and apparatus for fast action impulse thruster




Title: Methods and apparatus for fast action impulse thruster.
Abstract: Methods and apparatus for a fast action impulse thruster according to various aspects of the present invention may comprise a projectile comprising an impulse thruster system. The impulse thruster system may comprise a guidance system and a fast action impulse thruster system. The guidance system may control the trajectory of the projectile, for example by activating the fast action impulse thruster system to adjust the projectile's trajectory. The fast action impulse thruster system may be configured such that it may provide an impulse force to guide the projectile with a reaction time that is not affected by the rotational velocity of the projectile. The impulse force may be achieved by ejecting at least one mass from the projectile at high velocity such that a resulting momentum exchange may alter the trajectory of the projectile. The fast action impulse thruster system may also be configured in such a way so as to provide a significant improvement to the overall safety during the production, assembly, and handling of the projectile. ...


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USPTO Applicaton #: #20110309186
Inventors: Richard Dryer


The Patent Description & Claims data below is from USPTO Patent Application 20110309186, Methods and apparatus for fast action impulse thruster.




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stats Patent Info
Application #
US 20110309186 A1
Publish Date
12/22/2011
Document #
12389478
File Date
02/20/2009
USPTO Class
244/322
Other USPTO Classes
International Class
42B15/01
Drawings
3




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Raytheon Company


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Aeronautics And Astronautics   Missile Stabilization Or Trajectory Control   Automatic Guidance   Attitude Control Mechanisms   Fluid Reaction Type  

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20111222|20110309186|methods and fast action impulse thruster|Methods and apparatus for a fast action impulse thruster according to various aspects of the present invention may comprise a projectile comprising an impulse thruster system. The impulse thruster system may comprise a guidance system and a fast action impulse thruster system. The guidance system may control the trajectory of |Raytheon-Company
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