2,163 research outputs found
Aircraft electromagnetic compatibility
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
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
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)
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
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
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)
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
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
ΠΠ½ΡΠ΅Π³ΡΠ°ΡΠΈΡ Π½Π°Π½ΠΎΠΌΠ°ΡΠ΅ΡΠΈΠ°Π»ΠΎΠ² ΠΈΠ· Π³ΡΠ°ΡΠ΅Π½Π° Ρ ΠΏΡΠΈΠΌΠ΅Π½Π΅Π½ΠΈΠ΅ΠΌ 3D-ΠΏΠ΅ΡΠ°ΡΠΈ Π΄Π»Ρ Π±ΠΈΠΎΠΌΠ΅Π΄ΠΈΡΠΈΠ½ΡΠΊΠΈΡ ΠΈ ΡΠ΅Π½ΡΠΎΡΠ½ΡΡ ΠΏΡΠΈΠΌΠ΅Π½Π΅Π½ΠΈΠΉ
ΠΡΠΏΠΎΠ»ΡΠ·ΠΎΠ²Π°Π½ΠΈΠ΅ Π²ΠΎΡΡΡΠ°Π½ΠΎΠ²Π»Π΅Π½Π½ΡΡ
ΠΏΠ»Π΅Π½ΠΎΠΊ ΠΎΠΊΡΠΈΠ΄Π° Π³ΡΠ°ΡΠ΅Π½Π° Π΄Π»Ρ ΡΠΎΠ·Π΄Π°Π½ΠΈΡ ΠΏΠΎΠ»ΡΠΏΡΠΎΠ²ΠΎΠ΄Π½ΠΈΠΊΠΎΠ²ΡΡ
ΡΡΡΡΠΊΡΡΡ ΠΈ ΡΠ°Π·Π»ΠΈΡΠ½ΡΠ΅ ΠΏΡΠΎΠ²ΠΎΠ΄ΡΡΠΈΠ΅ ΠΏΠΎΠ²Π΅ΡΡ
Π½ΠΎΡΡΠΈ ΠΏΠΎΠΏΡΠ»ΡΡΠ½Ρ Π²ΠΎ Π²ΡΠ΅ΠΌ ΠΌΠΈΡΠ΅. Π ΠΎΠ»Ρ 3D-ΠΏΠ΅ΡΠ°ΡΠΈ
Π΄Π»Ρ ΡΠΎΠ·Π΄Π°Π½ΠΈΡ Π³ΠΈΠ±ΠΊΠΈΡ
ΡΡΡΡΠΊΡΡΡ ΠΎΡΡΠ°Π΅ΡΡΡ ΡΠΏΠΎΡΠ½ΡΠΌ. Π ΡΡΠΎΠΉ ΡΡΠ°ΡΡΠ΅ ΠΌΡ ΠΎΠ±ΡΠ΅Π΄ΠΈΠ½ΠΈΠ»ΠΈ ΡΡΠΈ
Π΄Π²Π΅ ΡΠ΅Ρ
Π½ΠΎΠ»ΠΎΠ³ΠΈΠΈ Π΄Π»Ρ ΠΈΠ·ΡΡΠ΅Π½ΠΈΡ Π³ΠΈΠ±ΠΊΠΎΠΉ ΡΠ»Π΅ΠΊΡΡΠΎΠ½ΠΈΠΊΠΈ Π½Π° ΠΎΡΠ½ΠΎΠ²Π΅ ΡΠΠ. ΠΠ°ΡΠΈ ΡΠ΅Π·ΡΠ»ΡΡΠ°ΡΡ ΠΏΠΎΠΊΠ°Π·ΡΠ²Π°ΡΡ, ΡΡΠΎ Π² Π·Π°Π²ΠΈΡΠΈΠΌΠΎΡΡΠΈ ΠΎΡ ΡΠ²ΠΎΠΉΡΡΠ² ΠΏΠΎΠ΄Π»ΠΎΠΆΠΊΠΈ ΠΈ ΡΠΏΠΎΡΠΎΠ±Π° ΠΎΠ±Π»ΡΡΠ΅Π½ΠΈΡ
ΠΎΠΊΡΠΈΠ΄Π° Π³ΡΠ°ΡΠ΅Π½Π°, ΠΌΠΎΠΆΠ½ΠΎ ΡΠΎΠ·Π΄Π°ΡΡ ΠΌΠ½ΠΎΠΆΠ΅ΡΡΠ²ΠΎ Π΄Π°ΡΡΠΈΠΊΠΎΠ² Ρ Π·Π°Π΄Π°Π½Π½ΡΠΌΠΈ ΡΠ²ΠΎΠΉΡΡΠ²Π°ΠΌΠΈ. ΠΡΠ°
Π΄ΠΎΠΊΡΠΌΠ΅Π½Ρ ΠΏΡΠ΅Π΄ΡΡΠ°Π²Π»ΡΠ΅Ρ ΡΠΎΠ±ΠΎΠΉ Π΄Π°ΡΡΠΈΠΊ ΡΠ΅ΠΌΠΏΠ΅ΡΠ°ΡΡΡΡ, Π΄Π°ΡΡΠΈΠΊ ΠΈΠ·Π³ΠΈΠ±Π° ΠΈ Π΄Π°ΡΡΠΈΠΊ Π²Π»Π°ΠΆΠ½ΠΎΡΡΠΈ Π΄Π»Ρ
ΠΏΡΠΎΠ΄Π΅ΠΌΠΎΠ½ΡΡΡΠΈΡΠΎΠ²Π°ΡΡ, ΠΊΠ°ΠΊ ΡΡΠΈ Π΄Π²Π΅ ΠΏΠ΅ΡΡΠΏΠ΅ΠΊΡΠΈΠ²Π½ΡΠ΅ ΡΠ΅Ρ
Π½ΠΎΠ»ΠΎΠ³ΠΈΠΈ ΠΌΠΎΠ³ΡΡ Π±ΡΡΡ ΠΎΠ±ΡΠ΅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
Instrumentation design study for testing a hypersonic ramjet engine on the x-15 a-2. volume 3- conceptual design of measurement systems
Instrumentation for testing hypersonic ramjet engine on X-15A-2 aircraf
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