IP Library Granted Patent US 8,464,640
Granted Patent B2
US 8,464,640 · App. 13/101,934 · Granted Jun 18, 2013

Controllable digital solid state cluster thrusters for rocket propulsion and gas generation

Inventor: Wayne N. Sawka (Reno, NV)
Assignee: Digital Solid State Propulsion LLC
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Quick Facts
Patent No.
US 8,464,640
App. No.
13/101,934
Granted
Jun 18, 2013
Kind
B2
Abstract

A thruster stack assembly and method for manufacturing the same is provided. The thruster stack assembly includes a plurality of grain elements having a common core region (e.g., a channel or passageway), where each grain element comprises a volume of electrically ignitable propellant. The thruster stack assembly further includes electrodes associated with the plurality of grain elements, the electrodes adapted for selectively igniting the plurality of grain elements. In one example, one or more of the grain elements may be ignited and combusted without igniting or damaging adjacent grain elements of the stack. The core region serves to channel combustion gases and exhaust from the thruster stack. Multiple stacks may be assembled together to form three-dimensional thruster arrays.

Claims (12)

1. A thruster stack assembly, comprising:

a plurality of grain elements having a common core region, each grain element comprising a volume of electrically ignitable propellant, wherein:

the electrically ignitable propellant is ignitable in response to the application of electrical power there through, and

the common core region comprises a passageway adjacent a portion of each of the plurality of grain elements for the passage of combustion gas; and

electrodes associated with the plurality of grain elements, the electrodes adapted for selectively igniting the plurality of grain elements.

2. The assembly of claim 1 , wherein an insulation layer is disposed between two adjacent grain elements.

3. The assembly of claim 1 , wherein an electrode is disposed between two adjacent grain elements.

4. The assembly of claim 1 , wherein two adjacent grain elements are disposed in direct contact with each other.

5. The assembly of claim 1 , wherein at least two grain elements comprise two coaxially aligned rings of the electrically ignitable propellant.

6. The assembly of claim 1 , further comprising a plurality of stacked thrusters, each thruster having a plurality of grain elements, thereby forming a three-dimensional array of addressable grain elements.

7. The assembly of claim 1 , wherein the common core region communicates with at least one exhaust port.

8. The assembly of claim 1 , wherein the plurality of grain elements are stacked along a vertical dimension and the common core region is disposed along the vertical dimension.

Assignments (2)
MERGER Recorded Dec 16, 2014
From: DIGITAL SOLID STATE PROPULSION, LLC
To: DIGITAL SOLID STATE PROPULSION, INC.
Reel/Frame 034519/0757 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 22, 2012
From: SAWKA, WAYNE N.
To: DIGITAL SOLID STATE PROPULSION LLC
Reel/Frame 027912/0319 →
Continuity (3)
Division 11305742 · Dec 16, 2005
Provisional Application 60637018 · Dec 17, 2004
Related Publication 20120137912A1 · Jun 7, 2012