The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Feb. 28, 2006

Filed:

Jan. 29, 2004
Applicants:

Mark Folsom, Carmel, CA (US);

Charles Piper, Iii, Los Banos, CA (US);

Wm. David Fahey, Cupertino, CA (US);

Jared M. Mcgowan, Boulder Creek, CA (US);

Inventors:

Mark Folsom, Carmel, CA (US);

Charles Piper, III, Los Banos, CA (US);

Wm. David Fahey, Cupertino, CA (US);

Jared M. McGowan, Boulder Creek, CA (US);

Assignee:

Quantic Industries, Inc., San Carlos, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F41G 7/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

The present invention provides a fast, low-cost, small diverter capable of generating a relatively high impulse (1-5 N-sec) over a short time period. The diverter is adapted for installation in a projectile for steering the projectile in flight by ejecting an end cap or hot burning gases in response to control signals from a guidance system. In one embodiment, multiple diverters are arranged in one or more bands about a flying projectile such as a rocket. Each diverter includes a header assembly providing support for a plurality of electrical leads, a mounting surface either on the header assembly or on a sealing assembly, a reactive semiconductor bridge mounted on the mounting surface and providing an electrical path for the electrical leads at a certain voltage across the bridge, a diverter body supporting the header assembly and containing a prime, wherein the reactive semiconductor bridge and the prime permit a gap, and an end cap or a sealing assembly attached to the diverter body containing the propellant.


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