Mainak Saha1,21Department of Metallurgical and Materials Engineering, National Institute of Technology, Durgapur-713209, India2Department of Metallurgical and Materials Engineering, Indian Institute of Technology Madras, Chennai-600036, IndiaAbstract - While descending through different layers of atmosphere with tremendously high velocities, hypersonic re-entry nosecones fabricated using ultra-high temperature ceramic matrix composites (UHTCMCs) are subjected to repeated thermal shocks. This necessitates extensive investigations on the cyclic oxidation behaviour of UHTCMCs at temperatures ranging from 1100°C to 1300°C (service temperature of the nosecones). To this end, the present work is aimed at investigating the cyclic oxidation behaviour of ZrB2 -20 vol.%MoSi2 (ZM20) UHTCMC (a very widely investigated ZM CMC) by carrying out cycles for 6h, at 1cycle/h and estimating oxidation kinetic law. This has been followed by extensive characterisation using X-Ray Diffraction (XRD) to indicate the phases formed during oxidation and Scanning electron microscopy-energy dispersive spectroscopy (SEM-EDS), in order to determine the chemical composition of the oxides formed between 1100°C and 1300°C.Keywords- Borides; ceramic composites; cyclic oxidation; kinetics; oxide layerAmong UHTCs, ZrB2-based ceramics have been reported to be potential candidates for the manufacture of reusable Thermal Protection Systems (TPS) in Hypersonic re-entry nosecones, due to very high thermal conductivity and relatively low density [1,2]. However, the low fracture toughness and poor thermal shock resistance of these ceramics pose major obstacles to their use in extreme environment [3]. Moreover, the poor oxidation resistance of ZrB2 at temperatures above 1200°C, due to formation of B2O3, and a non-protective porous scale of ZrO2 [4], poses restrictions to its use at elevated temperatures, especially above 1200°C. Thus, it becomes extremely important to find materials, which may highly enhance the oxidation resistance of ZrB2 [5-8]. A significant amount of work has already been done in that direction [8-12]. Besides, a significant amount of research has been done on reinforcing diborides like ZrB2, HfB2 and TiB2 with SiC, MoSi2, or ZrSi2 for enhanced oxidation resistance beyond 800°C [3- 23]. However, a limited amount of study has been made on cyclic oxidation of ZM20 at temperatures exceeding 1100°C, which is not at all unlikely, in the context of Hypersonic nosecones, during a high velocity descent through different layers of atmosphere. Thus, the scope of the present study is to investigate the cyclic oxidation behaviour of ZM20 between 1100 and 1300 °C.The important conclusions drawn from the results and discussions of this study have been elucidated. Cyclic oxidation behaviour of ZrB2-20 vol.% MoSi2 composite have been studied at 1100 °C, 1200 °C, 1250 °C and 1300 °C for 6hrs. Monitoring weight change and examining oxide scales draw following conclusions:(i) Weight gain for both the composites increased with increasing temperature and time. (ii) Weight gain occurred due to formation of ZrO2 and SiO2, at elevated temperatures. (iii) The main oxidation products were ZrO2, MoO3 and SiO2. (iv) At 1200 °C and above, the presence of SiC particles markedly improves the resistance to oxidation of the composite due to the formation of borosilicate glass.(v) Due to formation of oxide layer on the surface, the hardness of the samples i.e. its mechanical properties decreased from center to surface.(vi) The cyclic oxidation of the samples follow linear oxidation kinetics from 1100 to 1250 ºC while at 1300 ºC it follows parabolic oxidation kinetics due to the protective action of SiO2 above 1250 ºC.The results of the present study and their analyses lead to the following directions for future work: (i) The oxidation kinetics of the samples beyond 1300 ºC can be studied. (ii) Residual strain calculations can be carried out. (iii) Mathematical modelling study of the oxidation kinetics can be carried out. (iv) TEM study of the samples can be carried out for more precarious measurements. (v) Carrying out diffusion studies on oxide layer.AcknowledgementThe authors are grateful to the Department of Metallurgical and Materials Engineering, NIT Durgapur and Central Research Facility(CRF), IIT Kharagpur, for their support to carry out the work and hereby declare no conflict of interest.

Mainak Saha

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In materials research involving additive manufacturing (AM)-based techniques for fabrication of a wide variety of materials, the latest trend at present is to focus largely on 3D printing (3DP) of nanoceramics, which at present is highly challenging, from both fundamental and industrial viewpoints inspite of the tremendous versatility offered by these techniques in terms of addressing design complexities [1]-[6]. The two main reasons for the same are: (i) low density and (ii) poor mechanical properties of nanoceramic parts fabricated using 3DP techniques [7]-[9]. The fundamental reason behind the two aforementioned features of 3DP-fabricated nanoceramic parts is the huge extent of microstructural inhomogeneity arising primarily due to variation in cooling rates during 'point by point', 'line by line' or 'layer by layer' deposition methodology followed in 3DP techniques [10]-[16], leading to a number of defects in the microstructure [17], [18]. Moreover, the industrial application of nanoceramic parts manufactured using 3DP techniques, is rather limited, primarily owing to the high manufacturing cost associated with these nanoceramic parts. Although, in the last ten years, there has been a considerable volume of work on 3DP-based techniques for manufacturing ceramic parts with enhanced densities and improved mechanical properties, however, there is limited understanding on the correlation of microstructure of 3DP-fabriated nanoceramic components with the mechanical properties. On the other hand, in the recent decade, the 'correlative' methodology of characterising microstructures from micro to nanoscale, involving a number of different structural and chemical characterisation techniques, for the study of a number of defects ranging from the equilibrium point (or 0-D) to non-equilibrium volume (or 3-D) defects, has been hugely employed in a number of metallic materials [19]-[21]. This has completely revolutionised the understanding of structure-property correlation and microstructural defects in these materials and paved a whole new dimension towards a systematic correlation of structure (ranging from bulk to nano-scale) to a wide range range of properties in these materials. However, in the context of 3DP-fabricated nanoceramic parts, at present, there is hardly report on understanding structure-property correlation using the aforementioned methodology. The present review is aimed to review some of the most commonly used 3DP techniques for the fabrication of nanoceramics and provide an overview of the future perspectives, associated with the necessity towards developing a systematic structure-property correlation through 'correlative' characterisation methodology in these materials.

Mainak Saha

and 1 more

In materials research involving additive manufacturing (AM)-based techniques for fabrication of a wide variety of materials, the latest trend at present is to focus largely on 3D printing (3DP) of nanoceramics, which at present is highly challenging, from both fundamental and industrial viewpoints inspite of the tremendous versatility offered by these techniques in terms of addressing design complexities [1]-[6]. The two main reasons for the same are: (i) low density and (ii) poor mechanical properties of nanoceramic parts fabricated using 3DP techniques [7]-[9]. The fundamental reason behind the two aforementioned features of 3DP-fabricated nanoceramic parts is the huge extent of microstructural inhomogeneity arising primarily due to variation in cooling rates during 'point by point', 'line by line' or 'layer by layer' deposition methodology followed in 3DP techniques [10]-[16], leading to a number of defects in the microstructure [17], [18]. Moreover, the industrial application of nanoceramic parts manufactured using 3DP techniques, is rather limited, primarily owing to the high manufacturing cost associated with these nanoceramic parts. Although, in the last ten years, there has been a considerable volume of work on 3DP-based techniques for manufacturing ceramic parts with enhanced densities and improved mechanical properties, however, there is limited understanding on the correlation of microstructure of 3DP-fabriated nanoceramic components with the mechanical properties. On the other hand, in the recent decade, the 'correlative' methodology of characterising microstructures from micro to nanoscale, involving a number of different structural and chemical characterisation techniques, for the study of a number of defects ranging from the equilibrium point (or 0-D) to non-equilibrium volume (or 3-D) defects, has been hugely employed in a number of metallic materials [19]-[21]. This has completely revolutionised the understanding of structure-property correlation and microstructural defects in these materials and paved a whole new dimension towards a systematic correlation of structure (ranging from bulk to nano-scale) to a wide range range of properties in these materials. However, in the context of 3DP-fabricated nanoceramic parts, at present, there is hardly report on understanding structure-property correlation using the aforementioned methodology. The present review is aimed to review some of the most commonly used 3DP techniques for the fabrication of nanoceramics and provide an overview of the future perspectives, associated with the necessity towards developing a systematic structure-property correlation through 'correlative' characterisation methodology in these materials.

Mainak Saha

and 2 more