IP Library Granted Patent US 10,337,457
Granted Patent B2
US 10,337,457 · App. 15/572,535 · Granted Jul 2, 2019

Rocket motor with energetic grain having region with energetic disposed therein

Inventors: Michael D. Lynch (Rancho Cordova, CA); Richard Johnson (Rancho Cordova, CA)
Assignee: Aerojet Rocketdyne, Inc.
F02K9/12B29C64/165B33Y10/00B33Y70/00B33Y80/00C06D5/06F02K9/18F02K9/24B29K2027/06F05D2230/31
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Quick Facts
Patent No.
US 10,337,457
App. No.
15/572,535
Granted
Jul 2, 2019
Kind
B2
Abstract

A rocket motor ( 20 ) includes a nozzle ( 22 ) and a solid propellant section ( 24 ) in communication with the nozzle. The solid propellant section includes a first energetic grain layer ( 38, 32 ) that has a top surface and a bottom surface, and a second energetic grain layer ( 40, 44 ) that has a top surface and a bottom surface. The second layer is located on top of the first layer. The bottom surface of the second energetic grain layer partially abuts the top surface of the first energetic grain layer, and the bottom surface of the second energetic grain layer and the top surface of the first energetic grain layer define a region ( 46, 48 ) therebetween. A powder energetic ( 49 ) is disposed in the region.

Claims (10)

1. A solid propellant, comprising:

a first energetic grain layer having a top surface and a bottom surface;

a second energetic grain layer having a top surface and a bottom surface, the second layer on top of the first layer, wherein the bottom surface of the second energetic grain layer partially abuts the top surface of the first energetic grain layer, wherein the bottom surface of the second energetic grain layer and the top surface of the first energetic grain layer define a region there between; and

a powder energetic disposed in the region, wherein the powder energetic is a loose powder.

2. The solid propellant as recited in claim 1 , wherein the region is a micro-region.

3. The solid propellant as recited in claim 1 , wherein the powder energetic has a higher burn rate than the first energetic grain layer and the second energetic grain layer.

4. The solid propellant as recited in claim 1 , wherein the powder energetic substantially fills the region.

5. The solid propellant as recited in claim 1 , wherein the powder energetic partially fills the region such that there is open void space in the region.

6. The solid propellant as recited in claim 1 , wherein the region is a radially elongated slot.

7. The solid propellant as recited in claim 1 , wherein the first energetic grain layer includes the region and the second energetic grain layer is solid.

Assignments (3)
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 064424/0098 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Sep 27, 2018
From: AEROJET ROCKETDYNE, INC.
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 047570/0964 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 8, 2017
From: LYNCH, MICHAEL D.; JOHNSON, RICHARD
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 044069/0224 →
Continuity (2)
Provisional Application 62211601 · Aug 28, 2015
Related Publication 20180156158A1 · Jun 7, 2018
Cited By (1)
US 12,674,650