In-situ solid rocket motor propellant grain aging using liquid

Patent metadata

Field	Value
Publication number	US-11408377-B2
Application number	US-201916386169-A
Country	US
Kind code	B2
Filing date	Apr 16, 2019
Priority date	Apr 16, 2019
Publication date	Aug 9, 2022
Grant date	Aug 9, 2022

Abstract

A method for non-destructively determining a mechanical property of a solid rocket motor propellant grain may comprise applying a force to a surface of the solid rocket motor propellant grain, wherein a deformation is formed on the surface of the solid rocket motor propellant grain in response to the applying, and calculating a value of the mechanical property of the solid rocket motor propellant grain based on the deformation. The force may be applied by moving a liquid into the perforation. This process may be performed over time to determine a lifespan of the propellant grain.

First claim

What is claimed is:

1. A method for non-destructively aging a solid rocket motor propellant grain, wherein the solid rocket motor propellant grain comprises a solid mass with an exposed inner surface area defining a perforation in an interior of the solid rocket motor propellant grain, the method comprising:
moving a liquid into the perforation;
applying a force to a surface of the solid rocket motor propellant grain via the liquid, wherein a deformation is formed on the surface of the solid rocket motor propellant grain in response to the application of the force;
measuring at least one of a pressure of the liquid or a volume of the liquid; and
calculating a value of a mechanical property of the solid rocket motor propellant grain based upon the deformation, wherein the mechanical property comprises a bulk relaxation modulus (k) calculated using equation

k
=

P

Δ
⁢
V

V

i
⁢
n
⁢
i
⁢
t
⁢
i
⁢
a
⁢
l

,

where P is the measured pressure of the liquid, ΔV is a change in volume of the perforation, and V initial is an initial volume of the perforation.

2. The method of claim 1 , further comprising determining a lifespan of the solid rocket motor propellant grain based on at least one of the pressure of the liquid and the volume of the liquid.

3. The method of claim 1 , further comprising:
connecting a conduit to a port of the solid rocket motor propellant grain;
moving the liquid into the perforation, via the conduit, wherein the force is applied to the surface in response to the liquid being moved into the perforation of the solid rocket motor propellant grain; and
measuring the pressure of the liquid.

4. The method of claim 3 , further comprising pressurizing the liquid, wherein the deformation is formed in response to the liquid being pressurized.

5. The method of claim 4 , wherein a pre-determined volume of the liquid is moved into the perforation.

6. The method of claim 4 , wherein the liquid is moved into the perforation until the pressure of the liquid reaches a pre-determined value.

Assignees

• Goodrich Corp

Inventors

• Carter Joshua David
• Mueller Kevin

Classifications

• F05D2260/83

  Testing, e.g. methods, components or tools therefor · CPC title

• F02K9/08 Primary

  using solid propellants (F02K9/72 takes precedence; using semi-solid or pulverulent propellants F02K9/70) · CPC title

• F05D2300/501

  Elasticity · CPC title

• F05D2230/72

  Maintenance · CPC title

• F02K9/96 Primary

  characterised by specially adapted arrangements for testing or measuring · CPC title