Thermal barrier coatings for substrates comprising titanium. The thermal barrier coating may include a bond layer, an insulating layer, and a sealant layer. The bond layer may include titanium, a titanium alloy, an intermetallic compound of titanium, and/or a titanium metal matrix composite. The bond layer may have a superlattice structure having a periodically repeating group of layers. Methods for producing the thermal barrier coatings and articles of manufacture employing the thermal barrier coatings.
THERMAL PROTECTION SYSTEM FOR LIGHTWEIGHT HYPERSONIC MISSILE FIN
2021-07-22
Patent
Electronic Resource
English
Thermal protection system for lightweight hypersonic missile fin
European Patent Office | 2022
|THERMAL PROTECTION SYSTEM FOR LIGHTWEIGHT HYPERSONIC MISSILE FIN
European Patent Office | 2021
|Thermal protection system for lightweight hypersonic missile fin
European Patent Office | 2023
|Thermal protection system for lightweight hypersonic missile fin
European Patent Office | 2022
|Hypersonic Missile Propulsion System
NTIS | 1998
|