2,163 research outputs found

    Aircraft electromagnetic compatibility

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    Illustrated are aircraft architecture, electromagnetic interference environments, electromagnetic compatibility protection techniques, program specifications, tasks, and verification and validation procedures. The environment of 400 Hz power, electrical transients, and radio frequency fields are portrayed and related to thresholds of avionics electronics. Five layers of protection for avionics are defined. Recognition is given to some present day electromagnetic compatibility weaknesses and issues which serve to reemphasize the importance of EMC verification of equipment and parts, and their ultimate EMC validation on the aircraft. Proven standards of grounding, bonding, shielding, wiring, and packaging are laid out to help provide a foundation for a comprehensive approach to successful future aircraft design and an understanding of cost effective EMC in an aircraft setting

    Ultrasonic stress wave characterization of composite materials

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    The work reported covers three simultaneous projects. The first project was concerned with: (1) establishing the sensitivity of the acousto-ultrasonic method for evaluating subtle forms of damage development in cyclically loaded composite materials, (2) establishing the ability of the acousto-ultrasonic method for detecting initial material imperfections that lead to localized damage growth and final specimen failure, and (3) characteristics of the NBS/Proctor sensor/receiver for acousto-ultrasonic evaluation of laminated composite materials. The second project was concerned with examining the nature of the wave propagation that occurs during acoustic-ultrasonic evaluation of composite laminates and demonstrating the role of Lamb or plate wave modes and their utilization for characterizing composite laminates. The third project was concerned with the replacement of contact-type receiving piezotransducers with noncontacting laser-optical sensors for acousto-ultrasonic signal acquisition

    LDEF Materials Workshop 1991, part 2

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    The LDEF Materials Workshop 1991 was a follow-on to the Materials Sessions at the First LDEF Post-Retrieval Symposium held in Kissimmee, Florida, June 1991. The workshop comprised a series of technical sessions on materials themes, followed by theme panel meetings. Themes included materials, environmental parameters, and data bases; contamination; thermal control and protective coating and surface treatments; polymers and films; polymer matrix composites; metals, ceramics, and optical materials; lubricants adhesives, seals, fasteners, solar cells, and batteries. This document continues the LDEF Space Environmental Effects on Materials Special Investigation Group (MSIG) pursuit to investigate the effects of LEO exposure on materials which were not originally planned to be test specimens. Papers from the technical sessions are presented

    Technology for large space systems: A special bibliography with indexes (supplement 03)

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    A bibliography containing 217 abstracts addressing the technology for large space systems is presented. State of the art and advanced concepts concerning interactive analysis and design, structural concepts, control systems, electronics, advanced materials, assembly concepts, propulsion, solar power satellite systems, and flight experiments are represented

    Index to 1984 NASA Tech Briefs, volume 9, numbers 1-4

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    Short announcements of new technology derived from the R&D activities of NASA are presented. These briefs emphasize information considered likely to be transferrable across industrial, regional, or disciplinary lines and are issued to encourage commercial application. This index for 1984 Tech B Briefs contains abstracts and four indexes: subject, personal author, originating center, and Tech Brief Number. The following areas are covered: electronic components and circuits, electronic systems, physical sciences, materials, life sciences, mechanics, machinery, fabrication technology, and mathematics and information sciences

    Development of self-heating concrete for urban furniture by means of electrically conductive concrete

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    Mediante la utilizaciΓ³n de nuevos materiales es posible conferir a las estructuras de nuevas propiedades, como la capacidad autocalefactante. Mediante el uso de hormigones conductores se puede conseguir mediante la aplicaciΓ³n de una tensiΓ³n elΓ©ctrica incrementar la temperatura dada de un elemento de hormigΓ³n. El presente TFG aborda el desarrollo de elementos de mobiliario urbano calefactables empleando hormigΓ³n de altas prestaciones (UHPC) reforzado con fibra de carbono reciclada

    Technology for large space systems: A special bibliography with indexes (supplement 04)

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    This bibliography lists 259 reports, articles, and other documents introduced into the NASA scientific and technical information system between July 1, 1980 and December 31, 1980. Its purpose is to provide information to the researcher, manager, and designer in technology development and mission design in the area of the Large Space Systems Technology Program. Subject matter is grouped according to systems, interactive analysis and design. Structural concepts, control systems, electronics, advanced materials, assembly concepts, propulsion, solar power satellite systems, and flight experiments

    Study of wrap-rib antenna design

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    The results of a parametric design study conducted to develop the significant characteristics and technology limitations of space deployable antenna systems with aperture sizes ranging from 50 up to 300 m and F/D ratios between 0.5 and 3.0 are presented. Wrap/rib type reflectors of both the prime and offset fed geometry and associated feed support structures were considered. The significant constraints investigated as limitations on achievable aperture were inherent manufacturability, orbit dynamic and thermal stability, antenna weight, and antenna stowed volume. A data base, resulting in the defined maximum achievable aperture size as a function of diameter, frequency and estimated cost, was formed

    Π˜Π½Ρ‚Π΅Π³Ρ€Π°Ρ†ΠΈΡ Π½Π°Π½ΠΎΠΌΠ°Ρ‚Π΅Ρ€ΠΈΠ°Π»ΠΎΠ² ΠΈΠ· Π³Ρ€Π°Ρ„Π΅Π½Π° с ΠΏΡ€ΠΈΠΌΠ΅Π½Π΅Π½ΠΈΠ΅ΠΌ 3D-ΠΏΠ΅Ρ‡Π°Ρ‚ΠΈ для биомСдицинских ΠΈ сСнсорных ΠΏΡ€ΠΈΠΌΠ΅Π½Π΅Π½ΠΈΠΉ

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    ИспользованиС восстановлСнных ΠΏΠ»Π΅Π½ΠΎΠΊ оксида Π³Ρ€Π°Ρ„Π΅Π½Π° для создания ΠΏΠΎΠ»ΡƒΠΏΡ€ΠΎΠ²ΠΎΠ΄Π½ΠΈΠΊΠΎΠ²Ρ‹Ρ… структур ΠΈ Ρ€Π°Π·Π»ΠΈΡ‡Π½Ρ‹Π΅ проводящиС повСрхности популярны Π²ΠΎ всСм ΠΌΠΈΡ€Π΅. Роль 3D-ΠΏΠ΅Ρ‡Π°Ρ‚ΠΈ для создания Π³ΠΈΠ±ΠΊΠΈΡ… структур остаСтся спорным. Π’ этой ΡΡ‚Π°Ρ‚ΡŒΠ΅ ΠΌΡ‹ объСдинили эти Π΄Π²Π΅ Ρ‚Π΅Ρ…Π½ΠΎΠ»ΠΎΠ³ΠΈΠΈ для изучСния Π³ΠΈΠ±ΠΊΠΎΠΉ элСктроники Π½Π° основС Ρ€Π“Πž. Наши Ρ€Π΅Π·ΡƒΠ»ΡŒΡ‚Π°Ρ‚Ρ‹ ΠΏΠΎΠΊΠ°Π·Ρ‹Π²Π°ΡŽΡ‚, Ρ‡Ρ‚ΠΎ Π² зависимости ΠΎΡ‚ свойств ΠΏΠΎΠ΄Π»ΠΎΠΆΠΊΠΈ ΠΈ способа облучСния оксида Π³Ρ€Π°Ρ„Π΅Π½Π°, ΠΌΠΎΠΆΠ½ΠΎ ΡΠΎΠ·Π΄Π°Ρ‚ΡŒ мноТСство Π΄Π°Ρ‚Ρ‡ΠΈΠΊΠΎΠ² с Π·Π°Π΄Π°Π½Π½Ρ‹ΠΌΠΈ свойствами. Π­Ρ‚Π° Π΄ΠΎΠΊΡƒΠΌΠ΅Π½Ρ‚ прСдставляСт собой Π΄Π°Ρ‚Ρ‡ΠΈΠΊ Ρ‚Π΅ΠΌΠΏΠ΅Ρ€Π°Ρ‚ΡƒΡ€Ρ‹, Π΄Π°Ρ‚Ρ‡ΠΈΠΊ ΠΈΠ·Π³ΠΈΠ±Π° ΠΈ Π΄Π°Ρ‚Ρ‡ΠΈΠΊ влаТности для ΠΏΡ€ΠΎΠ΄Π΅ΠΌΠΎΠ½ΡΡ‚Ρ€ΠΈΡ€ΠΎΠ²Π°Ρ‚ΡŒ, ΠΊΠ°ΠΊ эти Π΄Π²Π΅ пСрспСктивныС Ρ‚Π΅Ρ…Π½ΠΎΠ»ΠΎΠ³ΠΈΠΈ ΠΌΠΎΠ³ΡƒΡ‚ Π±Ρ‹Ρ‚ΡŒ ΠΎΠ±ΡŠΠ΅Π΄ΠΈΠ½Π΅Π½Ρ‹.The use of reduced graphene oxide films to create semiconductor structures and various conductive surfaces is popular all over the world. The role of 3D printing to create flexible structures is still controversial. In this paper, we combined these two technologies to study flexible electronics based on rGO. Our results show that depending on the properties of the substrate and the method of irradiation of graphene oxide, it is possible to create many sensors with preset properties. This paper presents a temperature sensor, a bend sensor, and a humidity sensor to demonstrate how these two promising technologies can be combined
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