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Development and characterization of ultralow thermal conductivity Carbon Aerogel composites for space applications

Implementing Organization

Principal Investigator
Dr. KodandaRam Mangipudi
Indian Institute Of Technology Bhubaneswar, Odisha
kodanda@iitbbs.ac.in
CO-Principal Investigator
Prof. Venkataraman Sekkar
Cochin University Of Science And Technology, 26/226, University Road, Vidya Nagar Colony, Thrikkakara, Edappally, Kochi,Kerala,Ernakulam-682022
CO-Principal Investigator
Dr. V Sivanandan Achari
Cochin University Of Science And Technology,26/226, University Road, Vidya Nagar Colony, Thrikkakara, Edappally, Kochi,Kerala,Ernakulam-682022
CO-Principal Investigator
Dr. Vijayakrishna Kari
Indian Institute Of Technology Bhubaneswar,Argul - Jatni Road, Kansapada,Odisha,Khordha-752050

Project Overview

Space economy is projected as the future multitrillion dollar industry with space tourism, interstellar habitats, and space mining. Therefore, space science is a frontier with multitudes of technological and geopolitical opportunities and challenges. This applies to both civilian as well as defence applications. These space transportation vehicles, be it a space shuttle or a missile, with multiple re-entries into earth’s atmosphere are necessary which require a durable, ultralow thermal conductivity thermal protection systems (TPS) operating at high temperatures. High performance TPS materials that can also share some structural loads can potentially reduce to a weight reduction of 20 to 30%. Aerogels are more than 95% porous (light weight) and possess a very low thermal conductivity, and therefore are ideal candidate materials for TPS. However, these lack necessary mechanical strength to be used directly. Hence, we propose the fabrication of carbon foam and carbon felt/carbon aerogel composites. The studies includes optimizing the internal micro and mesostructure through controlling the process parameters to achieve low thermal conductivity composites. For oxidation resistance, it is proposed to coat the composite with SiC/ZrB2. Carbon foams with different pore sizes will be synthesized through the pyrolysis of commercially available polyurethane foams, while felts are commercially available. The carbon aerogel surrounding the reinforcement phase (C-foam/felt) will be formed by a sol-gel method using resorcinol-formaldehyde along with with sodium carbonate as the catalyst. Subsequent to the solvent exchange step, the hydrogel thus formed will be pyrolyzed to obtain carbon aerogel in the pores of carbon foam/felt. Detailed characterization of the composites will be performed using SEM, TEM, Raman, XRD, thermal conductivity measurements, and compression tests to optimize the micro and mesostructures of the composite for optimum thermos-mechanical properties for a durable low thermal conductivity composite material.
Funding Organization
Quick Information
Area of Research
Engineering Sciences
Focus Area
Mechanical & Manufacturing Engineering & Robotics
Start Date
21 May 2024
End Date
20 May 2027
Status
ongoing
Output
No. of Research Paper
00
Technologies (If Any)
00
No. of PhD Produced
00
Publications
00
No. of Patents
Filed : 00
Grant : 00
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