Flexible radiation shield

Patent metadata

Field	Value
Publication number	US-9640288-B1
Application number	US-201514954583-A
Country	US
Kind code	B1
Filing date	Nov 30, 2015
Priority date	Nov 30, 2015
Publication date	May 2, 2017
Grant date	May 2, 2017

Abstract

A pliable multilayer blanket configured as a particle radiation shield, the blanket including multiple layers. A first layer of the multiple layers is composed of a first material and a second layer of the multiple layers is composed of a second material, different from the first material, each layer being less than 20 mils thick. At least one of the first material and the second material is a metal or metal alloy having an atomic number (Z) of at least 29.

First claim

What is claimed is:

1. An apparatus comprising:
a pliable multilayer blanket configured as a particle radiation shield, the blanket including at least three layers, the at least three layers including at least one electrically nonconductive layer disposed between two electrically conductive layers, the pliable multilayer blanket including an electrically conductive coupling between the two electrically conductive layers of the pliable multilayer blanket for electrostatic discharge protection, wherein:
a first layer of the at least three layers is composed of a first material and a second layer of the multiple layers is composed of a second material, different from the first material, each layer being less than 20 mils thick; and
at least one of the first material and the second material is a metal or metal alloy having an atomic number (Z) of at least 29.

2. The apparatus of claim 1 , wherein the pliable multilayer blanket provides a particle radiation shielding to no worse than an aluminum panel having a thickness of 15 mils.

3. The apparatus of claim 2 , wherein the pliable multilayer blanket has a weight per unit area at least 10% less than the aluminum panel.

4. The apparatus of claim 1 , wherein at least one layer is attached, non-rigidly, to an adjacent layer.

5. The apparatus of claim 1 , wherein a flexible adhesive is disposed between the first layer and the second layer.

6. The apparatus of claim 1 , wherein the first material has a first Z value and the second material has a second Z value, the first Z value being less than or equal to 75% of the second Z value.

7. The apparatus claim 6 , wherein the first material is a non-metal and the second material is a nonmagnetic metal or nonmagnetic metal alloy.

8. The apparatus of claim 7 , wherein the first material is aluminum or a polyamide composite and the second material is copper, molybdenum, tin or tantalum.

9. The apparatus of claim 1 , wherein a total thickness of the pliable multilayer blanket is less than 30 mils.

10. The apparatus of claim 1 , wherein the electrically conductive coupling includes one or both of conductive insert and a thin conductive pattern disposed around edges of the multilayer blanket.

11. The apparatus of claim 1 , wherein a third layer is composed of one of the first material and the second material.

12. The apparatus of claim 1 , wherein a third layer is composed of a third material that is different from both the first material and the second material.

13. The apparatus of claim 1 , wherein the pliable multilayer blanket provides a radiation shielding no worse than an aluminum panel having a thickness of 28.5 mils.

14. The apparatus of claim 13 , wherein the pliable multilayer blanket has a mass per unit area at least 15% less than the aluminum panel.

15. A method comprising:
installing a particle radiation shield onto a spacecraft, wherein the particle radiation shield is formed from a pliable multilayer blanket, the blanket including at least three layers, the at least three layers including at least one electrically nonconductive layer disposed between two electrically conductive layers, the pliable multilayer blanket including a first electrically conductive coupling between the two electrically conductive layers of the pliable multilayer blanket for electrostatic discharge protection, wherein:
a first layer of the at least three layers is composed of a first material and a second layer of the multiple layers composed of a second material, different from the first material, each layer being less than 20 mils thick; and
at least one of the first material and the second material is a metal or metal alloy having atomic number (Z) of at least 29.

16. The method of claim 15 , wherein the first material has a first Z value and the second material has a second Z value, the first Z value being less than or equal to 75% of the second Z value, and installing the particle radiation shield includes disposing the pliable multilayer blanket on the spacecraft such that the first material is facing a direction from which incoming particle radiation is expected to arrive.

17. The method of claim 15 , wherein:
the first electrically conductive coupling includes one or both of a conductive insert and a thin conductive pattern disposed around edges of the multilayer blanket; and
installing the particle radiation shield includes providing a second electrically conductive coupling between the first electrically conductive coupling and an electrical ground point of the spacecraft.

18. The method of claim 15 , wherein installing the particle radiation shield includes cutting, from a bulk amount of multilayer sheet stock, a multilayer blanket having a shape defined by a planar pattern, and manually forming the multilayer blanket to fit around a spacecraft component.

Assignees

• Space Systems/Loral LLC

Inventors

• Wong Kit Pui Frankie

Classifications

• G21F3/00

  Shielding characterised by its physical form, e.g. granules, or shape of the material · CPC title

• G21F1/125 Primary

  comprising metals · CPC title

• B64G1/543

  protecting the crew in manned spacecraft · CPC title