U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Drag control module for stabilized projectiles

Patent 5762291 Issued on June 9, 1998. Estimated Expiration Date: Icon_subject September 5, 2017. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

1096907

1152668

1166879

1243542

1300708

2981183

3457862

3588004

Automatically deployed shell fins
Patent #: 4332360
Issued on: 06/01/1982
Inventor: Topliffe

Rocket fin hold down spring
Patent #: 4384691
Issued on: 05/24/1983
Inventor: Madderra

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Inventors

Assignee

Application

No. 924515 filed on 09/05/1997

US Classes:

244/3.24, Externally mounted stabilizing appendage (e.g., fin)244/3.21, Attitude control mechanisms244/3.25, Removable244/3.27Collapsible

Examiners

Primary: Jordan, Charles T.
Assistant: Wesson, Theresa M.

Attorney, Agent or Firm

International Class

F42B 010/00

Abstract

A trajectory (range) control device which is designed to fit behind the f of a fin stabilized ballistic projectile for correcting range error. The trajectory (range) control device is a self-contained, add-on module, which will screw into the forward portion of the projectile. The fuze will then screw into the trajectory (range) control module, which has a small through hole that will coincide with the center of the fuze and the center of the projectile. This through hole is intended to provide a channel in which the fuze can detonate the intended booster charge which will in turn ignite the high explosive payload or function the payload of the fin stabilized ballistic projectile. The trajectory control device will not make changes to the existing projectile or fuze. During the course correction phase, eight spring loaded flare tabs will deploy from the device. The flare tabs create a blunt cross-sectional area in front of the projectile, thus creating more drag and effectively slowing the projectile.

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