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Development of advanced thermal barrier coatings for high thrust rocket engines and components

Implementing Organization

CSIR-Central Electrochemical Research Institute, Karaikkudi, Tamil Nadu
Principal Investigator
Dr. Gosipathala Sreedhar
Scientist
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CSIR-Central Electrochemical Research Institute, Karaikkudi, Tamil Nadu
CO-Principal Investigator
Dr. SGK Manikandan
Mahendragiri, Tamil Nadu
ISRO Propulsion Complex

Project Overview

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.

Related Research

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Funding Organization
Funding Organization
Department of Space (DoS)
Quick Information
Area of Research
Astronomy & Space Sciences
Focus Area
Thermal Barrier Coatings
Start Year
2023
Sanction Amount
₹ 19.73 L
Status
Ongoing
Output
No. of Research Paper
00
Technologies (If Any)
00
No. of PhD Produced
N/A
Startup (If Any)
00
No. of Patents
Filed :00
Grant :00
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