Patent · US Active

Tail thruster control for projectiles

US8624171B2 · kind B2 · utility

5Cited by
13References
14Claims
0Family size

Assignee

Inventor

Key dates

Filing dateMar 9, 2011
Grant dateJan 7, 2014
Priority date
Expiry dateMar 9, 2031

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF42B10/666
  • WIPO fieldOther special machines
  • WIPO sectorMechanical engineering

Abstract

A system and method for guiding a projectile is presented. A nozzle system includes a boom assembly body that can be attached to a rear end of a projectile. A gas tank in the boom assembly contains pressurized gas. Fins are attached to the boom assembly body to guide the projectile. A valve lets a pulse of gas out of the gas tank. A nozzle expels the pulse of gas to control an angle of attack and lift of the projectile to guide the projectile to a target.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.