Development of advanced thermal barrier coatings for high thrust rocket engines and components
Implementing Organization
Principal Investigator
Dr. Gosipathala Sreedhar
Scientist
|
CSIR-Central Electrochemical Research Institute, Karaikkudi, Tamil Nadu
CO-Principal Investigator
Dr. SGK Manikandan
Mahendragiri, Tamil Nadu
ISRO Propulsion Complex
About
Conventional Thermal Barrier Coating (TBC) systems consist of a duplex structure with a metallic bond coat and a ceramic, heat-isolative topcoat. For thermal barrier coatings, potential materials like pyrochlore (e.g., La2Zr2O7,Gd2Zr2O7), spinel (MgAl2O4), perovskite (e.g., SrZrO3), or magnetoplumbite (e.g., LaMgAl11O19) structures are being explored. The necessary thermophysical and mechanical properties are being studied.
Achievements
The project being undertaken by ISRO in collaboration with academia is directly or indirectly beneficial to the society.
Source
Source
Indian Space Research Organisation (ISRO)- Department of Space (DOS) 2022-2045
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