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"Polymer composites are increasingly used in aerospace applications due to properties such as strength and durability compared to weight. Edited by two leading authorities in the field, this book summarises key recent research on design, manufacture and performance of composite components for aerospace structures. Part one reviews the design and manufacture of different types of composite component. Part two discusses aspects of performance such as stiffness, strength, fatigue, impact and blast behaviour, response to temperature and humidity as well as non-destructive testing and monitoring techniques."

"Sensors and Instrumentation, Volume 8. Proceedings of the 36th IMAC, A Conference and Exposition on Structural Dynamics, 2018, the eighth volume of nine from the Conference brings together contributions to this important area of research and engineering. The collection presents early findings and case studies on fundamental and applied aspects of Sensors and Instrumentation, including papers on; Sensor Applications, Accelerometer Design, Accelerometer Calibration, Sensor Technology, Energy Harvesting Technology, and Aircraft/Aerospace Technology"

"This book shows step-by-step examples of the physical arguments and the resulting calculations obtained using the quick-fire method. Also demonstrate the estimation improvements that can be obtained through the use of more detailed physics-based back-of-the-envelope engineering models. These different methods are used to obtain the solutions to a number of design and performance estimation problems arising from two of the most complex real-world engineering projects : the space shuttle and the hubble space telescope satellite."

"Saat ini, karena masalah lingkungan, ketersediaan dan keterbaruan, pengembangan komposit polimer berpenguat serat alam meningkat. Serat kenaf Sumberejo merupakan salah satu serat alam yang melimpah di Indonesia. Penelitian ini bertujuan untuk memperoleh sifat mekanik komposit berpenguat serat kenaf Sumberejo anyam menggunakan model analitik dengan memvariasikan jenis polimer pada komposit. Orientasi serat anyam dengan perlakuan alkali adalah 0^o/90^o. Polimer yang digunakan adalah polimer termoset (epoksi dan vinil ester) dan termoplastik (polipropilena dan poli asam laktat). Rule of Mixtures (ROM) dan Teori Lamina diterapkan sebagai model analitik. Hasil menunjukkan bahwa nilai modulus tarik, kuat tarik longitudinal, kuat tarik transversal, modulus geser, dan kuat geser komposit tertinggi terdapat pada komposit epoksi berpenguat serat kenaf Sumberejo, masing-masing yaitu 6,58 GPa, 131,04 MPa, 114,93 MPa, 1,78 GPa, dan 8,92 MPa. Mengacu pada Standar Nasional Indonesia 01-4449-2006 tentang papan serat komposit, keempat komposit polimer berpenguat serat kenaf Sumberejo anyam 0^o/90^o digolongkan sebagai papan serat kerapatan tinggi.

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Nowadays, due to environmental concerns, availability and renewable issues, the development of natural fiber reinforced polymer composites is increasing. Sumberejo kenaf fiber is one of the abundant natural fibers in Indonesia. The purpose of this study was to obtain the mechanical properties of woven Sumberejo kenaf fiber composite using analytical models by varying the types of polymers in the composite. The orientation of the woven alkaline-treated fiber was 0^o/90^o. Polymers used were thermosets (epoxy and vinyl esters) and thermoplastics (polypropylene and polylactic acid). Rule of Mixtures (ROM) and Lamina Theory were applied for the analytical model. The results showed that the highest value of tensile modulus, longitudinal tensile strength, transverse tensile strength, shear modulus, and shear strength were found in Sumberejo kenaf fiber reinforced epoxy composite, 6,58 GPa, 131,04 MPa, 114,93 MPa, 1,78 GPa, and 8,92 MPa respectively. Referring to Indonesian National Standard 01-4449-2006 for composite fiber board, four 0^o/90^o woven Sumberejo kenaf fiber reinforced polymer composites were classified as high density fiber board."

"Powered flight : the engineering of aerospace propulsion aims to provide a broader context, allowing observations and comparisons to be made across systems that are overlooked by focusing on a single aspect alone. The physics and history of aerospace propulsion are built on step-by-step, coupled with the development of an appreciation for the mathematics involved in the science and engineering of propulsion. Powered flight : the engineering of aerospace propulsion covers its subject matter both theoretically and with an awareness of the practicalities of the industry. To ensure that the content is clear, representative but also interesting the text is complimented by a range of relevant graphs and photographs including representative engineering, in addition to several propeller performance charts."

"Dewasa ini, penggunaan material komposit polimer berpenguat serat karbon (carbon fiber reinforced polymer, CFRP) dalam berbagai bidang semakin populer dan berkembang. Hal ini dikarenakan nilai ekonomis serta sifat mekanik yang baik yang mampu dihasilkan oleh material komposit tersebut. Ada banyak faktor yang dapat mempengaruhi sifat/ karakteristik material komposit CFRP, diantaranya adalah arah orientasi serat karbon serta perlakuan panas. Penelitian ini membahas mengenai pengaruh orientasi serat anyam karbon dan temperatur perlakuan panas terhadap sifat mekanik material komposit laminate bermatrik polimer. Komposit CFRP dimanufaktur dengan menggunakan metode hand lay-up dengan variasi orientasi [00 or 900]s, [00 or 900]/[±450] dan [±450]s. Spesimen komposit selanjutnya dilakukan pemanasan pada variasi temperatur lalu dilakukan pengujian berupa pengujian tarik, tekuk, impak, dan FTIR. Kekuatan tarik tertinggi diperoleh pada orientasi [0o or 90o]s dengan pemanasan 200 oC selama 3 jam, kekuatan tekuk tertinggi diperoleh pada orientasi [0o or 90o]s dengan pemanasan 100 oC selama 3 jam, serta energi impak tertinggi diperoleh pada orientasi [0o or 90o]s dengan pemanasan 100 oC selama 3 jam. Hasil pengujian FTIR menunujukkan gugus fungsi polimer yang dihasilkan dari Unsaturated Polyester Resin setelah pemanasan pada temperature curing adalah ikatan C=O (ester) dan ikatan ikatan C=C (cincin aromatik).

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Nowadays, the use of carbon fiber reinforced polymer (CFRP) composite in various fields is getting more popular and fast growing. This is due to the economic value and good mechanical properties of the composite materials can produce. There are many factors that affect the characteristics of CFRP composite materials, including orientation of the carbon fiber and heat treatment. This study discusses the effect of the orientation of carbon woven fibers and the temperature of heat treatment on the mechanical properties of polymer matrix composite laminates. CFRP composites were manufactured using the hand lay-up method with various orientations [0 or 90o]s, [0 or 90o] / [± 45o] and [± 45o]s. The composite specimens were then heating at various temperatures. Characteristics of the composites were examined in the form of tensile test, bending test, impact test and FTIR analysis. The highest tensile strength was obtained at orientation [0o or 90o]s followed by heating at 200 oC for 3 hours. The highest bending strength was obtained at orientation [0o or 90o]s followed by heating at 100 oC for 3 hours, whereas the highest impact energy was obtained at orientation [0o or 90o]s followed by heating at 100 oC for 3 hours. FTIR test showed that the polymer functional groups from unsaturated polyester resin after heating at curing temperature are C=O bonds (ester) and C=C bonds (aromatic rings)."

"This book presents high-quality contributions in the subject area of Aerospace System Science and Engineering, including topics such as: Trans-space vehicle systems design and integration, Air vehicle systems, Space vehicle systems, Near-space vehicle systems, Opto-electronic system, Aerospace robotics and unmanned system, Aerospace robotics and unmanned system, Communication, navigation and surveillance, Dynamics and control, Intelligent sensing and Information fusion, Aerodynamics and aircraft design, Aerospace propulsion, Avionics system, Air traffic management, Earth observation, Deep space exploration, Bionic micro-aircraft/spacecraft.The book is a selection of articles from the 2nd International Conference on Aerospace System Science and Engineering, held in Moscow, Russia, from 31 July to 1 August 2018. The conference is co-organized by Shanghai Jiao Tong University and Moscow Aviation Institute. This is a forum that brings together experts in astronautics and aeronautics to share new ideas and findings. "