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Dynamic thermal management system for aerospace avionics in extreme atmospheric conditions

Patent #US12945234B2

Public record:Verify on Google Patents

This cooling system employs a micro-capillary phase-change loop to regulate the temperature of sensitive navigation computers. It ensures operational reliability during high-altitude thermal cycling.

Issue Date

4/15/2026

Inventor

Hiroshi Tanaka

Seller Location

United States

Price on request

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