Layered Oxidant-Resistant Cover With Integrated Light Reflection

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Solution Overview

Problem

Existing space hardware protection methods against atmospheric oxidants like atomic oxygen and sulfuric acid are limited to single-material coatings, which do not allow for tailored protection levels and often require additional light reflectors, increasing mass and complexity.

Innovation Solution

A cover comprising multiple layers of different atmospheric oxidant-resistant materials, including glass, silver, and adhesive layers, with integrated optical surface reflectors, allowing for controlled protection and reduced temperature through light reflection, without needing additional reflectors.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If single-material coatings are used for protection against atmospheric oxidants, then the protection is uniform and simple to apply, but the protection level cannot be tailored and additional light reflectors are needed increasing mass and complexity

Engineering Contradiction:
Improvecustomizable protection levelVSAvoidstructure complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The cover is segmented into multiple layers (first layer with oxidant-resistant materials, second layer with reflective materials, third layer with conductive materials) rather than using a single uniform coating. This segmentation allows each layer to perform its specific function while collectively providing customizable protection levels against atmospheric oxidants.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention uses composite material structures where different materials are combined in specific layers. The first layer combines oxidant-resistant materials, the second layer combines reflective materials, and the third layer combines conductive materials. This composite approach enables tailored protection while integrating multiple functions into a unified structure.

Inventive Principle:
Principle #40Composite materials

2Temperature

If additional light reflectors are added for temperature reduction, then the temperature control improves, but the mass and complexity increase

Engineering Contradiction:
Improvetemperature reductionVSAvoidmass
Core Design Contradiction:
TemperatureVSWeight of moving object

Solution Approach 1:

The reflective function is merged into the second layer of the cover structure itself, rather than being a separate component. The reflective materials in the second layer are integrated with the oxidant-resistant first layer and conductive third layer, creating a multi-functional cover that reduces temperature without requiring additional separate reflectors.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The cover structure is designed as a universal multi-functional system where the layered structure simultaneously provides oxidant protection, temperature control through light reflection, and electrical conductivity. This multi-functionality eliminates the need for separate dedicated components for each function, reducing overall mass and complexity.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Provides customizable protection against atmospheric oxidants, reduces temperature effects, and minimizes mass by integrating reflectivity, eliminating the need for separate reflectors.

Implementation Method 1

the third material is reflective... By reflecting part of the light, the temperature of the cover can be reduced significantly

Methodology Applied
Scientific EffectLight reflection: Reflection

Data Source

PatentEP4541718B1Cover for protection against an atmospheric oxidant
Publication Date: 2025.12.03 AIRBUS DEFENCE & SPACE GMBH
  • EP4541718B1 patent drawingFigure 1
  • EP4541718B1 patent drawingFigure 2
  • EP4541718B1 patent drawingFigure 3

AI summary

A cover (1a; 1b; 1c, figures 4a-4c) for protection of space hardware (13, figures 4a-4c) against an atmospheric oxidant, wherein the cover (1a; 1b; 1c, figures 4a-4c) comprises: a first layer (A), which has one side configured to face away from space hardware (13, figures 4a-4c) and an opposite side configured to face towards space hardware (13, figures 4a-4c), comprising: at least one first material portion (3), and at least one second material portion (5), wherein the first material and the second material are different atmospheric oxidant resistant materials. A method for manufacturing the cover (1a; 1b; 1c, figures 4a-4c).