VO2 Thermochromic Coating for Passive Space Thermal Control

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Solution Overview

Problem

Current thermal control methods for space platforms are hindered by significant size, weight, and power (SWAP) impacts, and existing radiative thermal control solutions using VO2-based dynamic coatings have not achieved the desired thermal emissivity targets for passive thermal control.

Innovation Solution

A multi-layer coating comprising a thermochromic VO2 layer and long-wave infrared dielectrics in a reflective configuration, which changes thermal emissivity by altering the substrate temperature through the VO2 phase-change transition temperature, allowing for a low SWAP approach to thermal control.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If active heat source/sink systems (heating: resistive, radioisotope/cooling: thermoelectric, fluid loop) are used for thermal control, then thermal control effectiveness is improved, but size, weight, and power (SWAP) impacts increase significantly

Engineering Contradiction:
Improvethermal control effectivenessVSAvoidSWAP
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The patent replaces active mechanical thermal control systems (fluid loops, thermoelectric coolers) with a passive optical/thermal system using VO2-based dynamic coatings that automatically adjust thermal emissivity in response to temperature changes, eliminating the need for heavy mechanical actuators and fluid management hardware

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The patent changes the thermal emissivity parameter of the coating dynamically through temperature-induced phase transitions of VO2 material, allowing the system to adapt its thermal control characteristics without adding physical mass or power consumption

Inventive Principle:
Principle #35Parameter changes

2Weight of moving object

If passive thermal control by radiation control using actuated louvres or passive bimorph louvres is used, then SWAP advantages are provided, but device complexity increases

Engineering Contradiction:
ImproveSWAPVSAvoidcomplexity
Core Design Contradiction:
Weight of moving objectVSDevice complexity

Solution Approach 1:

The patent extracts the thermal control function from complex mechanical assemblies (louvres with actuators, bimorph structures) and concentrates it into a simple coating layer that performs thermal regulation through inherent material phase transitions, eliminating mechanical complexity while maintaining SWAP advantages

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The VO2-based coating automatically adjusts its thermal emissivity in response to temperature changes without requiring external control systems, actuators, or complex mechanisms, achieving self-regulating thermal control that is both simple and lightweight

Inventive Principle:
Principle #25Self-service

3Adaptability or versatility

If VO2-based dynamic coatings are used for radiative thermal control, then thermal control capability is provided, but thermal emissivity targets (Cold TE≥0.85) are not achieved

Engineering Contradiction:
Improvethermal control capabilityVSAvoidthermal emissivity target
Core Design Contradiction:
Adaptability or versatilityVSManufacturing precision

Solution Approach 1:

The patent uses composite material structures combining VO2 with other dielectric and metallic layers to achieve both the desired thermal control capability and the specific thermal emissivity target of Cold TE≥0.85, overcoming the limitations of simple VO2 coatings through optimized multi-layer configurations

Inventive Principle:
Principle #40Composite materials

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

The coating achieves a significant change in thermal emissivity, enabling effective passive thermal control by switching between low and high emissivity states, thus efficiently managing temperature fluctuations in space platforms with simplicity, robustness, and low SWAP characteristics.

Implementation Method 1

The coating produces a change in surface thermal absorptance, and total emissivity, as the coating substrate temperature passes through the thermochromic phase-change transition temperature.

Methodology Applied
Scientific EffectPhase change: Phase Change

Implementation Method 2

a switchable TE is achieved by a multi-layer coating comprising thermochromics (in one aspect VO2 is used)

Methodology Applied
Scientific EffectThermochromism: Thermochromism

Implementation Method 3

Radiative thermal control using VO2-based dynamic coatings

Methodology Applied
Scientific EffectThermal radiation: Thermal Radiation

Implementation Method 4

long-wave infrared films, in a reflective configuration

Methodology Applied
Scientific EffectReflection: Reflection

Data Source

PatentUS20240343924A1Variable thermal emissivity coating and method
Publication Date: 2024.10.17 TELEDYNE SCIENTIFIC & IMAGING LLC
  • US20240343924A1 patent drawing
  • US20240343924A1 patent drawing
  • US20240343924A1 patent drawing

AI summary

A coating comprising a first dielectric overlayer, a first dielectric underlayer, a continuous thermochromic layer disposed between the first dielectric overlayer and the first dielectric underlayer, and a metal layer disposed below the first dielectric underlayer.