Coating capables of resisting to high thermal stress and particularly to coatings for satellites and spatial vessels and to methods for producing those coatings

• US 4,663,234 A
• Filed: 11/09/1984
• Issued: 05/05/1987
• Est. Priority Date: 03/11/1983
• Status: Expired due to Fees

• Current Assignee: Agence Spatiale Europeenne
• Original Assignee: Agence Spatiale Europeenne
• Inventors: Bouton, Francois A.
• Primary Examiner(s): Herbert, Thomas J.
• Application Number:
  US06/680,259
• Time in Patent Office: 907 Days
• Field of Search: 428/35, 428/422, 428/457, 428/699, 428/701, 244/163, 427/250, 427/252, 427/248.1
• US Class Current: 428/422
• CPC Class Codes: B64G 1/226 Special coatings for spacecraft
• CPC Class Codes: B64G 1/58 Thermal protection, e.g. heat shields
• CPC Class Codes: Y10T 428/31544 Addition polymer is perhalogenated
• CPC Class Codes: Y10T 428/31678 Of metal

Abstract

A composite coating for objects subjected to high thermal stresses.

This composite coating comprises a first layer made of a material suitable for ensuring heat control, an intermediate layer made of a transparent, amorphous inorganic substance insensitive to water and alcohol, and a third layer, or outer layer, made of a conducting transparent material, the coefficient of thermal expansion of the transparent, amorphous inorganic substance forming the intermediate layer being between the coefficients of thermal expansion of the materials forming the first and third layers of the composite coating. A process for the production of a composite coating of this type.

Application to satellites and spacecrafts.

Claims

1. A composite coating for an object subjected to high thermal stress, comprising a first inner layer made of a thermal control material, a second intermediate layer made of a transparent amorphous inorganic material which is insensitive to the action of water or alcohol, and a third outer layer made of a transparent conducting material, wherein the coefficient of thermal expansion of the said transparent amorphous inorganic substance forming the intermediate layer is between the coefficient of thermal expansion of the materials forming the said first and the said third layers of the composite coating.

2. The composite coating of claim 1, wherein the said layer made of a thermal control material is made of a fluorinated ethylene-propylene polymer.

3. A composite coating for a satellite, comprising a first inner layer made of a thermal control material, a second intermediate layer made of a transparent amorphous inorganic material insensitive to the action of water or alcohol, and a third outer layer made of a transparent conducting material, wherein the coefficient of thermal expansion of the transparent amorphous inorganic substance forming the intermediate layer is between the coefficient of thermal expansion of the materials forming the said first and the said third layers of the composite coating.

4. In a composite coating for an object subjected to high thermal stress, said composite coating containing:

(i) as an inner layer a second-surface mirror suitable for ensuring thermal control of the said object and comprising a dielectric material, the rear face of which is coated with a reflective material, and

(ii) an outer layer made of a conducting material for protection against electrostatic charging of the said object surface, the improvement comprising;

(iii) an intermediate layer made of an amorphous inorganic material preventing crack formation in the said conducting layer due to thermal cycling, which amorphous inorganic material has a coefficient of thermal expansion which is between the coefficient of thermal expansion of the said dielectric material and the said outer layer, respectively, and wherein the said amorphous inorganic material is not sensitive to the action of water and alcohol, said amorphous inorganic material being at least one member selected from the group consisting of metal oxides, lithium fluoride, and sodium fluoride.

5. In a composite coating for an object subjected to high thermal stress, said composite coating containing:

(i) as an inner layer a second-surface mirror suitable for ensuring thermal control of the said object and comprising a dielectric material, the rear face of which is coated with a reflective material, and

(ii) an outer layer made of a conducting material for protection against electrostatic charging of the said object'"'"'s surface, the improvement comprising;

(iii) an intermediate layer situated between the said inner layer and the said outer layer, said intermediate layer being made of an amorphous inorganic material preventing crack formation in the said conducting layer due to thermal cycling, which amorphous inorganic material has a coefficient of thermal expansion which is between the coefficients of thermal expansion of the said dielectric material and the said outer layer, respectively, and wherein the said amorphous inorganic material is not sensitive to the action of water and alcohol.

6. The composite coating of claim 5, wherein the said intermediate layer comprises a material which is at least one member selected from the group consisting of Bi₂ O₃, SiO₂, GeO₂, WO₃, Ga₂ O₃, Sb₂ O₃, TeO₂, LiF, NaF and mixtures thereof.

7. The composite coating of claim 6, wherein the said material is Bi₂ O₃.