High efficiency erosion resistant silicone ablator composition

Patent metadata

Field	Value
Publication number	US-9458356-B2
Application number	US-201414317920-A
Country	US
Kind code	B2
Filing date	Jun 27, 2014
Priority date	Jun 27, 2014
Publication date	Oct 4, 2016
Grant date	Oct 4, 2016

Abstract

A lightweight ablator formulation has been developed which offers superior thermal performance compared to current state of the art ablator formulations. The lightweight ablator formulations described herein typically include at least one endothermically decomposing (energy absorbing) material with a fluxing agent resulting in significantly reduced backface temperature response and a more stable surface. According to one implementation the ablator composition comprises about 30 to about 70 percent by weight of a base silicone resin, about 25 to about 67 percent by weight of a low-density filler, about 3 to about 7 percent by weight of a curing agent and greater than 0 and up to about 10 percent by weight of a boron-containing compound.

First claim

What is claimed is:

1. An ablator composition for providing ablation protection after cure thereof, comprising:
about 30 to about 70 percent by weight of a base silicone resin;
about 25 to about 67 percent by weight of a low-density filler having a bulk density between approximately 0.1 g/cc and 0.50 g/cc;
about 3 to about 7 percent by weight of a curing agent;
4.02 percent by weight of boric acid; and
4.02 percent by weight of ammonium phosphate dibasic.

2. The ablator composition of claim 1 , further comprising:
greater than 0 and up to about 20 percent by weight of a thinning fluid.

3. The ablator composition of claim 1 , wherein the low-density filler comprises silica microballoons.

4. The ablator composition of claim 1 , wherein the density of an ablator material formed by curing the ablator composition ranges between at least 0.3 and about 0.6 g/cc.

5. The ablator composition of claim 1 , wherein the tensile strength of an ablator material formed by curing the ablator composition is greater than about 689 kPa up to about 2068 kPa.

6. The ablator composition of claim 1 , further comprising a honeycomb core, wherein the honeycomb core provides increased surface area.

7. The ablator composition of claim 1 , further comprising a woven material, wherein the woven material provides increased surface area.

8. The ablator composition of claim 1 , further comprising a non-woven material, wherein the non-woven material provides increased surface area.

9. A method of forming an ablative structure, the method comprising:
(a) forming an ablator composition by mixing:
about 30 to about 70 percent by weight of a base silicone resin;
about 25 to about 67 percent by weight of a low-density filler having a bulk density between approximately 0.1 g/cc and 0.50 g/cc;
about 3 to about 7 percent by weight of a curing agent;
4.02 percent by weight of boric acid; and
4.02 percent by weight of ammonium phosphate dibasic;

(b) forming the ablator composition into a geometrical shape; and
(c) curing the geometrical shape.

10. The method of claim 9 , wherein forming the ablator composition into a geometrical shape comprises at least one of the following: die molding of the ablator composition, extrusion of the ablator composition, manual application of the ablator composition, and spraying the ablator composition onto a surface.

11. The method of claim 10 , further comprising applying a coupling agent to the surface prior to spraying to enhance bonding between the ablator composition and the surface.

12. The method of claim 9 , further comprising scoring the ablative structure.

13. A method of mixing a low-density ablator composition, the method comprising:
(a) placing approximately 30 to about 70 percent by weight of a base silicone resin into a container;
(b) mixing approximately 3-7 percent by weight of a curing agent with the base silicone resin;
(c) mixing 4.02 percent by weight of boric acid and 4.02 percent by weight of ammonium phosphate dibasic with the resulting mixture of (b);
(d) mixing approximately 25-67 percent by weight of a low-density filler material with the resulting mixture of (c).

Assignees

• Boeing Co

Inventors

• Courter Kelly Jonathan
• Mobers Patrick Jacob
• Brewer Bryan

Classifications

• C09D183/04 Primary

  Polysiloxanes · CPC title

• B64G1/62

  Systems for re-entry into the earth's atmosphere; Retarding or landing devices · CPC title

• C08K2003/387

  Borates · CPC title

• C08K7/28

  Glass · CPC title

• B64G1/58

  Thermal protection, e.g. heat shields · CPC title