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1

Afaf M. Abd El-Hameed and Y. A. Abdel-Aziz. "Aluminium Alloys in Space Applications: A Short Report." Journal of Advanced Research in Applied Sciences and Engineering Technology 22, no. 1 (2021): 1–7. http://dx.doi.org/10.37934/araset.22.1.17.

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Because of the unique combination of light weight, high strength, and ease of fabrication, aluminum alloys have the mainstay of the aerospace industry. This report provides a brief overview of the types and series of aluminum alloys “AA” used for space industries and aerospace applications such as spacecraft surface structures and both of aircraft construction and satellite subsystems. The alloy compositions, manufacturing processes, and treatment classify the alloy properties and characteristics. According to these characteristics alloy compositions, the report outlines how to identify the su
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2

Sharma, A. K. "Gold plating on aluminium alloys for space applications." Transactions of the IMF 67, no. 1 (1989): 87–88. http://dx.doi.org/10.1080/00202967.1989.11870848.

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3

Busby, J. T., K. J. Leonard, and S. J. Zinkle. "Radiation-damage in molybdenum–rhenium alloys for space reactor applications." Journal of Nuclear Materials 366, no. 3 (2007): 388–406. http://dx.doi.org/10.1016/j.jnucmat.2007.03.028.

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4

Molinari, Alberto, Mario Zadra, Nério Vicente Jr., Luca Facchini, and Francesco Bucciotti. "Spark Plasma Sintering of Titanium Alloys for Biomedical Applications." Key Engineering Materials 704 (August 2016): 360–65. http://dx.doi.org/10.4028/www.scientific.net/kem.704.360.

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A dense Ti6Al4V with a porous cp2-Ti surface layer was produced by Spark Plasma Sintering, using a Calcium Phosphate powder as space holder. The duplex porosity structure resulting from the space holder (large pores) and the uncompleted densification of the titanium powder (micrometric pores) has a very positive effect on both cell in-growth and cell proliferation.The porous structure decreases the fatigue resistance significantly, even if less than what reported in literature, likely due to the formation of a globular microstructure in the interface region of the substrate, where fatigue crac
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5

Sharma, A. K., H. Bhojraj, V. K. Kaila, and H. Narayanamurthy. "Anodizing and inorganic black coloring of aluminum alloys for space applications." Metal Finishing 95, no. 12 (1997): 14–20. http://dx.doi.org/10.1016/s0026-0576(97)82621-9.

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6

Callahan, Patrick G., McLean P. Echlin, Jean Charles Stinville, et al. "Three-dimensional texture visualization approaches: applications to nickel and titanium alloys." Journal of Applied Crystallography 50, no. 5 (2017): 1267–79. http://dx.doi.org/10.1107/s1600576717010470.

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This paper applies the three-dimensional visualization techniques explored theoretically by Callahan, Echlin, Pollock, Singh & De Graef [J. Appl. Cryst.(2017),50, 430–440] to a series of experimentally acquired texture data sets, namely a sharp cube texture in a single-crystal Ni-based superalloy, a sharp Goss texture in single-crystal Nb, a random texture in a powder metallurgy polycrystalline René 88-DT alloy and a rolled plate texture in Ti-6Al-4V. Three-dimensional visualizations are shown (and made available as movies as supplementary material) using the Rodrigues, Euler and three-dim
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7

Mediaswanti, Kun, Vi Khanh Truong, Jafar Hasan, et al. "Fabrication of Ti14Nb4Sn Alloys for Bone Tissue Engineering Applications." Key Engineering Materials 520 (August 2012): 214–19. http://dx.doi.org/10.4028/www.scientific.net/kem.520.214.

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In this paper, porous Ti14Nb4Sn alloys were fabricated using a space holder sintering method, resulting in a porosity of ~70%. Scanning electron microscopy (SEM) analyses revealed a combination of both macropore and micropore structures. The fabricated titanium alloy scaffolds exhibited a similar structure to that of natural bone, which is expected to improve bone implant longevity. Bacterial cells of Pseudomonas aeruginosa ATCC 9027 were employed for the in vitro test.
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McCarthy, Tyler T., Zheng Ju, Stephen Schaefer, Shui-Qing Yu, and Yong-Hang Zhang. "Momentum(k)-space carrier separation using SiGeSn alloys for photodetector applications." Journal of Applied Physics 130, no. 22 (2021): 223102. http://dx.doi.org/10.1063/5.0063179.

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9

Somasundaram, Soniya, and P. Murali Krishna. "Anodization of Aluminium Alloys in Hydrofluoric Acid and Sulfuric Acid for Space Applications." Asian Journal of Chemistry 34, no. 10 (2022): 2763–70. http://dx.doi.org/10.14233/ajchem.2022.24029.

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Present work demonstrated the development of a typical solar reflector coating by optimizing the bath parameters for an anodizing process on aluminium 2024 alloy. This evidently explains the pre-cleaning as well as optimization of the bath parameters for the development of solar reflector anodic film on aluminium alloys. The electrolytic bath for anodization consists of concentrated sulphuric acid and hydrofluoric acid. The anodization parameters such as solution temperature, process time and current density were optimized in order to achieve an anodic film of 10-12 μm thickness on the alumini
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10

López-Ferreño, I., U. Urrutia, P. Lorenzo, et al. "Ultra-High-vacuum Experimental Equipment to Characterize Shape Memory Alloys for Space Applications." Materials Today: Proceedings 2 (2015): S953—S956. http://dx.doi.org/10.1016/j.matpr.2015.08.001.

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11

Muneshwar, Pravin, S. K. Singh, Bhanu Pant, S. C. Sharma, and M. C. Mittal. "Advanced processing techniques for titanium base alloys and its aluminides for space applications." Transactions of the Indian Institute of Metals 61, no. 2-3 (2008): 77–85. http://dx.doi.org/10.1007/s12666-008-0008-3.

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12

Matuszewski, Leszek. "Application of Shape Memory Alloys in Pipeline Couplings for Shipbuilding." Polish Maritime Research 27, no. 3 (2020): 82–88. http://dx.doi.org/10.2478/pomr-2020-0049.

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AbstractThe aim of the study is to analyse shape memory alloy (SMA) pipeline joints in limited space applications for all kinds of ships. Generally, the space available in various areas on ships is strictly limited and service works usually meet many obstacles. If we consider a pipeline, the flange joints always require a larger free space around the pipe than the pipe alone. A simultaneous problem can occur with the propeller shaft line coupling between bearings. SMA couplings require less space around the pipe and service should be easier, e.g., insulation fixing, painting and so on. SMA cou
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13

Bridges, Denzel, David Fieser, Jannira J. Santiago, and Anming Hu. "Novel Frontiers in High-Entropy Alloys." Metals 13, no. 7 (2023): 1193. http://dx.doi.org/10.3390/met13071193.

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There is little doubt that there is significant potential for high-entropy alloys (HEAs) in cryogenic and aerospace applications. However, given the immense design space for HEAs, there is much more to be explored. This review will focus on four areas of application for HEAs that receive less attention. These focus areas include joining technologies, HEA nanomaterial synthesis, catalysis, and marine applications. The performance of HEAs as a filler metal for welding and brazing as well as their performance as a welded/brazed base metal will be discussed. Various methods for synthesizing HEA na
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14

Nag, Soumya, Brian Jordan, Ke An, Jaimie Tiley, Chuan Zhang, and Fan Zhang. "Exploring Gradient Pathways in High Temperature, Functionally Graded Alloys." AM&P Technical Articles 180, no. 2 (2022): 16–20. http://dx.doi.org/10.31399/asm.amp.2022-02.p016.

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15

BANERJEE, RUDRA, and ABHIJIT MOOKERJEE. "AUGMENTED SPACE RECURSION CODE AND APPLICATION IN SIMPLE BINARY METALLIC ALLOY." International Journal of Modern Physics C 21, no. 02 (2010): 205–20. http://dx.doi.org/10.1142/s0129183110015051.

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We present here an optimized and parallelized version of the augmented space recursion code for the calculation of the electronic and magnetic properties of bulk disordered alloys, surfaces and interfaces, either flat, corrugated or rough, and random networks. Applications have been made to bulk disordered alloys to benchmark our code.
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16

Young, Rebecca C., William J. Buttner, Bruce R. Linnell, and Rajeshuni Ramesham. "Electronic nose for space program applications." Sensors and Actuators B: Chemical 93, no. 1-3 (2003): 7–16. http://dx.doi.org/10.1016/s0925-4005(03)00338-1.

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17

Troeger, L. P., Marcia S. Domack, and John A. Wagner. "Microstructural and Mechanical Characterization of Shear Formed Aluminum Alloys for Airframe and Space Applications." Materials Science Forum 331-337 (May 2000): 489–94. http://dx.doi.org/10.4028/www.scientific.net/msf.331-337.489.

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18

Ramesh Narayanan, P., Satyam Suwas, K. Sreekumar, Parameshwar Prasad Sinha, and Srinivasa Ranganathan. "Evolution of Crystallographic Texture in Cold Rolled Al-Zn-Mg Alloys Used in Space Applications." Materials Science Forum 702-703 (December 2011): 315–19. http://dx.doi.org/10.4028/www.scientific.net/msf.702-703.315.

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The aerospace industry uses a variety of materials in different forms like sheets, forgings, extruded rods, welded components and machined components for launch vehicle and satellite applications. As lighter and stronger materials are the aims of the aerospace industry, aluminium alloys are the most widely used materials in the in the aircraft and aerospace industries. These aluminum alloys used in the aerospace industry are subjected to a variety of processing operations, either in the sheet form after rolling, forging, heat treatment and machining conditions, to realize the final product imp
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19

Tuissi, Ausonio, Paola Bassani, and Carlo Alberto Biffi. "CuZnAl Shape Memory Alloys Foams." Advances in Science and Technology 78 (September 2012): 31–39. http://dx.doi.org/10.4028/www.scientific.net/ast.78.31.

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Foams and other highly porous metallic materials with cellular structures are known to have many interesting combinations of physical and mechanical properties. That makes these systems very attractive for both structural and functional applications. Cellular metals can be produced by several methods including liquid infiltration of leachable space holders. In this contribution, results on metal foams of Cu based shape memory alloys (SMAs) processed by molten metal infiltration of SiO2 particles are presented. By using this route, highly homogeneous CuZnAl SMA foams with a spherical open-cell
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20

David, S. A., R. G. Miller, and Z. Feng. "Welding of unique and advanced alloys for space and high-temperature applications: welding and weldability of iridium and platinum alloys." Science and Technology of Welding and Joining 22, no. 3 (2016): 244–56. http://dx.doi.org/10.1080/13621718.2016.1222255.

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21

Sunderland, Andrew, Alexey V. Veryaskin, Wayne McRae, Li Ju, and David G. Blair. "Direct string magnetic gradiometer for space applications." Sensors and Actuators A: Physical 147, no. 2 (2008): 529–35. http://dx.doi.org/10.1016/j.sna.2008.06.014.

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22

Anil Kumar, V., R. K. Gupta, M. J. N. V. Prasad, and S. V. S. Narayana Murty. "Recent advances in processing of titanium alloys and titanium aluminides for space applications: A review." Journal of Materials Research 36, no. 3 (2021): 689–716. http://dx.doi.org/10.1557/s43578-021-00104-w.

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23

Rioja, Roberto J. "Fabrication methods to manufacture isotropic Al-Li alloys and products for space and aerospace applications." Materials Science and Engineering: A 257, no. 1 (1998): 100–107. http://dx.doi.org/10.1016/s0921-5093(98)00827-2.

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24

Ramesh Narayanan, P., Satyam Suwas, K. Sreekumar, Parameshwar Prasad Sinha, and Srinivasa Ranganathan. "Influence of Crystallographic Texture on Mechanical Properties in Cold Rolled 7XXX Series Al Alloys Used in Space Applications." Materials Science Forum 710 (January 2012): 539–44. http://dx.doi.org/10.4028/www.scientific.net/msf.710.539.

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This paper covers the influence of crystallographic texture on the mechanical properties in two of the most important high strength Al-Zn-Mg family of aluminium alloys, viz., AA7075 and AFNOR7020 alloys, used in the Aerospace industry. AFNOR7020 Alloy developed a stronger texture compared to the other two alloys. S component of texture is stronger in AA7075 alloy whereas the Bs component is stronger in AFNOR7020 alloy. This is attributed to the shear banding which was found absent in the other alloy. The starting material, AA7075 in T7352 condition and AFNOR7020 in T652 condition show some deg
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25

Xia, Ji, Yuki Noguchi, Xiao Xu, et al. "Iron-based superelastic alloys with near-constant critical stress temperature dependence." Science 369, no. 6505 (2020): 855–58. http://dx.doi.org/10.1126/science.abc1590.

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Shape memory alloys recover their original shape after deformation, making them useful for a variety of specialized applications. Superelastic behavior begins at the critical stress, which tends to increase with increasing temperature for metal shape memory alloys. Temperature dependence is a common feature that often restricts the use of metal shape memory alloys in applications. We discovered an iron-based superelastic alloy system in which the critical stress can be optimized. Our Fe-Mn-Al-Cr-Ni alloys have a controllable temperature dependence that goes from positive to negative, depending
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26

Warner, Timothy. "Recently-Developed Aluminium Solutions for Aerospace Applications." Materials Science Forum 519-521 (July 2006): 1271–78. http://dx.doi.org/10.4028/www.scientific.net/msf.519-521.1271.

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Two principal approaches are available to materials’ engineers to improve the overall cost-weight balance of metallic airframe structures: improving alloy performance and optimising materials’ utilisation. Although both approaches have been successful in the past, they are most effective when applied concomitantly. The Aluminium industry has a long record of improving aerospace alloys’ performance. Nevertheless, even in apparently well-explored alloy systems such as the 7xxx family, products with improved damage tolerance-strength balances have recently been developed, thanks to an improved un
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27

Poroś, Dariusz, Stanisław Zaborski, and Paweł Karolczak. "Heat affected zone analysis of Ti6Al4V after WEDM." Mechanik 92, no. 12 (2019): 833–35. http://dx.doi.org/10.17814/mechanik.2019.12.115.

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Perspectives of applications WEDM for cutting titanium alloys are presented. There is space to explore how application of proper time parameters and the material of wire electrode for WEDM of titanium alloys affects the surface roughness, structure, the stress and the chemical composition of the formed surface layer.
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28

Leonard, Keith J., Jeremy T. Busby, and Steven J. Zinkle. "Aging effects on microstructural and mechanical properties of select refractory metal alloys for space-reactor applications." Journal of Nuclear Materials 366, no. 3 (2007): 336–52. http://dx.doi.org/10.1016/j.jnucmat.2007.03.025.

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29

Murphy, A. G., P. Meagher, A. Norman, and D. J. Browne. "Mechanical and thermal stability of Bulk Metallic Glass alloys identified as candidates for space mechanism applications." Materials & Design 224 (December 2022): 111350. http://dx.doi.org/10.1016/j.matdes.2022.111350.

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30

Mishra, Akshansh, and Devarrishi Dixit. "Friction Stir Welding of Aerospace Alloys." Journal of Mechanical Engineering 48, no. 1 (2019): 37–46. http://dx.doi.org/10.3329/jme.v48i1.41093.

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Friction Stir Welding (FSW) is a solid state joining process which possesses a great potential to revolutionise the aerospace industries. Distinctive materials are selected as aerospace alloys to withstand higher temperature and loads. Sometimes these alloys are difficult to join by a conventional welding process but they are easily welded by FSW process. The FSW process in aerospace applications can be used for: aviation for fuel tanks, repair of faulty welds, cryogenic fuel tanks for space vehicles. Eclipse Aviation, for example, has reported dramatic production cost reductions with FSW when
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31

Manikandan, S. G. K., M. Kamaraj, and C. Jebasihamony. "Review on Self-Healing Thermal Barrier Coatings for Space Applications." Materials Performance and Characterization 10, no. 1 (2021): 20210062. http://dx.doi.org/10.1520/mpc20210062.

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32

Bhasha, Sanjeev Gautam, Parul Malik, and Purnima Jain. "Ceramic Composites for Aerospace Applications." Diffusion Foundations 23 (August 2019): 31–39. http://dx.doi.org/10.4028/www.scientific.net/df.23.31.

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Ceramic composites is playing crucial role to accomplish highly efficiently and cost effective equipment for aerospace industry. The instigation of ceramics into aircraft industry is a promising step towards virtuous future. Ceramics has a key role in innovation of highly competent material for space travel which is highly economical and environmentally sustainable. Advancement in making fuel efficient engines are necessity in present scenario due to the harmful emissions releases in the environment by burning of fuel to power up engine. The high temperature application of composites makes it
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33

Bidulsky, Robert, and Juraj Seman. "KOSICE SELF-GOVERNING REGION AND THEIR INTERNATIONAL COOPERATION IN THE AREAS OF THE SPACE INDUSTRY AND AVIATION." Acta Metallurgica Slovaca 26, no. 4 (2020): 138–40. http://dx.doi.org/10.36547/ams.26.4.762.

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The main idea of the co-organize the Slovak space tech day and Slovak aviation industry days was to prove the position of Košice self-governing region (KSK), as a space in which suitable conditions are created for development in the areas of the space industry and aviation. The basis is a long-term historical context in the form of educational and research institutions in the KSK, as well as their involvement in international cooperation projects. KSK intended to declare demand for investments and international cooperation in the areas of the space industry and aviation. The given industries h
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34

Costanza, Girolamo, and Maria Elisa Tata. "Shape Memory Alloys for Aerospace, Recent Developments, and New Applications: A Short Review." Materials 13, no. 8 (2020): 1856. http://dx.doi.org/10.3390/ma13081856.

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Shape memory alloys (SMAs) show a particular behavior that is the ability to recuperate the original shape while heating above specific critical temperatures (shape memory effect) or to withstand high deformations recoverable while unloading (pseudoelasticity). In many cases the SMAs play the actuator’s role. Starting from the origin of the shape memory effect, the mechanical properties of these alloys are illustrated. This paper presents a review of SMAs applications in the aerospace field with particular emphasis on morphing wings (experimental and modeling), tailoring of the orientation and
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35

Böhnke, Tobias, Marika Edoff, and Lars Stenmark. "Development of a MOEMS sun sensor for space applications." Sensors and Actuators A: Physical 130-131 (August 2006): 28–36. http://dx.doi.org/10.1016/j.sna.2005.09.025.

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36

Dirri, Fabrizio, Ernesto Palomba, Andrea Longobardo, Emiliano Zampetti, Bortolino Saggin, and Diego Scaccabarozzi. "A review of quartz crystal microbalances for space applications." Sensors and Actuators A: Physical 287 (March 2019): 48–75. http://dx.doi.org/10.1016/j.sna.2018.12.035.

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37

Arrigoni, Michel. "Metallic Materials and Their Applications in Aerospace and Advanced Technologies." Metals 12, no. 2 (2022): 226. http://dx.doi.org/10.3390/met12020226.

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Exploring the mysteries of the universe, transporting people over longer distances in the safest way, providing energy to a growing global population, and facing environmental changes are among the major challenges that will face humanity in the coming decades: Satellite observations have become essential in monitoring the ecological health of the Earth, but they require space launches that raise the paradox of greenhouse and toxic gases rejection by the use of solid propellants [...]
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38

Chaieb, Oussama, Oluwole A. Olufayo, Victor Songmene, and Mohammad Jahazi. "Investigation on Surface Quality of a Rapidly Solidified Al–50%Si Alloy Component for Deep-Space Applications." Materials 13, no. 15 (2020): 3412. http://dx.doi.org/10.3390/ma13153412.

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To meet the requirements for high-performance products, the aerospace industry increasingly needs to assess the behavior of new and advanced materials during manufacturing processes and to ensure they possess adequate machinability, as well as high performance and an extensive lifecycles. Over the years, industrial research works have focused on developing new alloys with an increased thermal conductivity as well as increased strength. High silicon content aluminum (Al–Si) alloys, due to their increased thermal conductivity, low coefficient of thermal expansion, and low density, have been iden
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Nakaş, G. Ipek, Emin Erkan Aşik, Bensu Tunca, and Şakir Bor. "Fatigue and Fracture Behavior of Porous TiNi Alloys." Materials Science Forum 783-786 (May 2014): 591–96. http://dx.doi.org/10.4028/www.scientific.net/msf.783-786.591.

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While the wide range of applications of TiNi alloys make them highly appealing due to their shape memory and superelasticity properties, production of TiNi in the porous form further enlarges their application fields. Porous TiNi alloys have been studied extensively for biomedical applications due to their elastic modulus similar to that of bone. Accordingly, TiNi foams have been widely characterized in terms of their various mechanical properties; however, their fatigue properties have not been well studied, even though, it has a vital importance in structural applications such as medical imp
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40

Henslee, Allan M., Sarita R. Shah, Mark E. Wong, Antonios G. Mikos, and F. Kurtis Kasper. "Degradable, antibiotic releasing poly(propylene fumarate)-based constructs for craniofacial space maintenance applications." Journal of Biomedical Materials Research Part A 103, no. 4 (2014): 1485–97. http://dx.doi.org/10.1002/jbm.a.35288.

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41

Wang, Frank Fan, William McKeague, and Christina Polwarth. "Comparisons of Soldering Alloys in Large Ceramic Substrate to Metal Heatsink Attachment Application." International Symposium on Microelectronics 2018, no. 1 (2018): 000596–601. http://dx.doi.org/10.4071/2380-4505-2018.1.000596.

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Abstract Tin-lead alloys have historically been popular in the electronics industry for use in solder-attach applications. Despite recent restrictions related to lead content, some industries continue to use lead based alloys in solder applications. Tin-lead based alloys, in particular, have proven to have excellent solderability to tin, nickel, copper, gold, and silver metallization surfaces. They have also performed better in reliability than most of the lead free solders. As a result of this, they are still widely used in the aerospace and military electronics industry. Hybrid microelectron
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42

Czerwinski, Frank. "Thermal Stability of Aluminum Alloys." Materials 13, no. 15 (2020): 3441. http://dx.doi.org/10.3390/ma13153441.

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Thermal stability, determining the material ability of retaining its properties at required temperatures over extended service time, is becoming the next frontier for aluminum alloys. Its improvement would substantially expand their range of structural applications, especially in automotive and aerospace industries. This report explains the fundamentals of thermal stability; definitions, the properties involved; and the deterioration indicators during thermal/thermomechanical exposures, including an impact of accidental fire, and testing techniques. For individual classes of alloys, efforts ai
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43

Zuo, H. J., M. W. Price, R. D. Griffin, R. A. Andrews, and G. M. Janowski. "The effect of back-melting on the continuity of crystallographic orientation and composition in HgZnTe." Proceedings, annual meeting, Electron Microscopy Society of America 50, no. 2 (1992): 1696–97. http://dx.doi.org/10.1017/s0424820100133114.

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The II-VI semiconducting alloys, such as mercury zinc telluride (MZT), have become the materials of choice for numerous infrared detection applications. However, compositional inhomogeneities and crystallographic imperfections adversly affect the performance of MZT infrared detectors. One source of imperfections in MZT is gravity-induced convection during directional solidification. Crystal growth experiments conducted in space should minimize gravity-induced convection and thereby the density of related crystallographic defects. The limited amount of time available during Space Shuttle experi
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44

Matin, P. H., L. M. Smith, and S. Petrusevski. "A method for stress space forming limit diagram construction for aluminum alloys." Journal of Materials Processing Technology 174, no. 1-3 (2006): 258–65. http://dx.doi.org/10.1016/j.jmatprotec.2006.01.008.

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45

Lobanov, L. M., A. I. Ustinov, V. S. Volkov, A. A. Mokhniuk, V. A. Telichko, and S. A. Demchenkov. "Al/TiO2 bilayer coatings for space applications: Mechanical and thermoradiation properties." Thin Solid Films 668 (December 2018): 30–37. http://dx.doi.org/10.1016/j.tsf.2018.10.017.

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46

Hall, Ernest L. "The role of microscopy in the development of Ti-based intermetallic alloys." Proceedings, annual meeting, Electron Microscopy Society of America 50, no. 1 (1992): 164–65. http://dx.doi.org/10.1017/s0424820100121223.

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For the past two decades there has been interest in the development of Ti-based intermetallic alloys for aircraft structural and engine applications, culminating in intense activity over the past five years. The primary driver for this interest is the increase of the strength/weight ratio for aircraft materials, and the low density, high modulus, and high melting temperature of some Ti alloys make them promising candidates. Most of the work has centered on the Ti-Al system, particularly Ti3Al (ordered DO19 structure, space group P63/mmc), TiAl (ordered Ll0, space group P4/mmm), and, more recen
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47

Lethole, Ndanduleni, Phuti Ngoepe, and Hasani Chauke. "Compositional Dependence of Magnetocrystalline Anisotropy, Magnetic Moments, and Energetic and Electronic Properties on Fe-Pt Alloys." Materials 15, no. 16 (2022): 5679. http://dx.doi.org/10.3390/ma15165679.

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This work reported the first-principles calculations for the compositional dependence of the energetic, electronic, and magnetic properties of the bimetallic Fe-Pt alloys at ambient conditions. These hybrid alloys have gained substantial attention for their potential industrial applications, due to their outstanding magnetic and structural properties. They possess high magnetocrystalline anisotropy, density, and coercivity. Four Fe-Pt alloys, distinguished by compositions and space groups, were considered in this study, namely P4/mmm-FePt, I4/mmm-Fe3Pt, Pm-3m-Fe3Pt, and Pm-3m-FePt3. The calcul
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48

Maloy, Stuart A. "A Tem Study of Slip Systems in MoSi2/WSi2 Alloys." Proceedings, annual meeting, Electron Microscopy Society of America 49 (August 1991): 942–43. http://dx.doi.org/10.1017/s0424820100089020.

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MoSi2 has recently been investigated as a potential material for high temperature structural applications. It has excellent oxidation resistance up to 1700°C, a high melting temperature, 2030°C, and a brittle-to-ductile transition temperature at 900-1000°C. WSi2 is isomorphous with MoSi2 and has a body-centered tetragonal unit cell of the space group 14/mmm. The lattice parameters are a=3.20 Å and c=7.84 Å for MoSi2 and a=3.21 Å and c=7.88 Å for WSi2. Therefore, WSi2 was added to MoSi2 to improve its strength via solid solution hardening. The purpose of this study was to investigate the slip s
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49

Abidi, Irfan Haider, and Fazal Ahmad Khalid. "Sintering and Morphology of Porous Structure in NiTi Shape Memory Alloys for Biomedical Applications." Advanced Materials Research 570 (September 2012): 87–95. http://dx.doi.org/10.4028/www.scientific.net/amr.570.87.

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The combination of attractive properties of porous NiTi shape memory alloys like high recoverable strain due to superelasticity and shape memory effect, good corrosion resistance, improved biocompatibilty, low density and stiffness along with its porous structure similar to that of bone make them best materials for biomedical implants. In current study porous NiTi SMAs have been fabricated successfully by space holder technique via pressureless sintering using NaCl powder as a spacer. Various volume fractions of NaCl powders have been involved to study their effect on the pore characteristics
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50

Săndulache, Florin, Sergiu Stanciu, Nicanor Cimpoeşu, Ramona Cimpoeşu, and Teodor Stanciu. "Obtaining of Fe-Base Biodegradable Metallic Alloy." Key Engineering Materials 750 (August 2017): 175–79. http://dx.doi.org/10.4028/www.scientific.net/kem.750.175.

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Biodegradable metallic materials gain space in implantable materials field based on the applications that can fulfill. Beside Mg-based alloys a new class of metallic materials is under development, alloys based on Fe, in order to improve the corrosion rate, one of the disadvantages of magnesium alloys, and the mechanical properties of the implant. In this article we present the steps took to obtain a biodegradable FeMnSi alloy with metallic additions and few preliminary results about the chemical composition (X-ray dispersive energy analyze EDS) of the sample and the influence of hardening hea
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