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310-092 - Sun Cert Bus Component Developer Java EE Platform 5, Upgrade - Dump Information

Vendor : SUN
Exam Code : 310-092
Exam Name : Sun Cert Bus Component Developer Java EE Platform 5, Upgrade
Questions and Answers : 150 Q & A
Updated On : October 12, 2018
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310-092 Sun Cert Bus Component Developer Java EE Platform 5, Upgrade

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310-092 exam Dumps Source : Sun Cert Bus Component Developer Java EE Platform 5, Upgrade

Test Code : 310-092
Test Name : Sun Cert Bus Component Developer Java EE Platform 5, Upgrade
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Q&A : 150 Real Questions

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  Mariner 10 backup

Mariner 10 backup putting within the national Air and area Museum. within the mid-Seventies this flight-certified spacecraft became proposed for a Mercury orbiting mission that became now not accepted. (credit: Dwayne Day)

by using Dwayne A. DayMonday, October 8, 2018 Bookmark and Share

Later this month, if all goes to devise, the eu space agency will launch the BepiColombo spacecraft toward Mercury, the place it's going to arrive in December 2025. BepiColombo carries two spacecraft with a purpose to circle the planet, one specializing in Mercury’s floor and the other discovering its magnetosphere. The spacecraft is named after Giuseppe “Bepi” Colombo, an Italian scientist, mathematician, and engineer at the college of Padua, Italy who calculated the way to get a spacecraft into a resonant orbit with Mercury enabling dissimilar flybys. His method changed into used for the a success NASA Mariner 10 mission which flew previous Mercury in 1975.

looking on the mission summaries produced by way of JPL four a long time in the past, it's obvious that many of the spacecraft that NASA later constructed—like Magellan, Galileo, even Curiosity—had been either first proposed or appreciably sophisticated within the early-mid-1970s.

but flybys simplest supplied constrained data about Mercury, and what scientists wanted changed into to orbit the planet. the first inspiration to ship a spacecraft into Mercury orbit was made within the mid-Nineteen Seventies, but it was no longer unless the mid-1980s that a Jet Propulsion Laboratory trajectory specialist figured out a means to get a spacecraft into Mercury orbit with decent-sized payload, and only in 2011 did NASA at last accomplish that intention. In between, there have been lots of experiences and recommendations, as a variety of scientists and engineers tried to work out the finest means of getting a spacecraft to a tiny, quick planet inconveniently near a extremely hot ball of fuel.

sizzling summer

in the summer of 1974, the countrywide research Council’s area Science Board held a series of meetings of its element panels such because the Committee on Planetary and Lunar Exploration, or advanced. advanced become assigned the task of reviewing possible planetary missions for the next decade.

In preparation for this recreation, the Jet Propulsion Laboratory performed almost a dozen particular person reviews of new planetary missions, some of them primarily based upon existing spacecraft designs adapted for new missions, and others requiring fully new spacecraft. Two of the experiences concentrated on the deliberate arrival of the comet Encke in 1980, one mission worried a Venus orbital imaging radar, one other a solar electric powered out-of-the-ecliptic probe. other missions concentrated on Mars, including a polar orbiter, pattern return, and a Mars rover. a few missions have been for a Jupiter/Uranus flyby with Uranus atmospheric probe, and a Jupiter orbiter. looking at the mission summaries produced by way of JPL four decades in the past, it is evident that many of the spacecraft that NASA later developed—like Magellan, Galileo, even Curiosity—have been both first proposed or significantly refined within the early-mid-1970s.

a type of 1974 mission proposals was for a “Mariner Mercury Orbiter 1978,” a spacecraft that can be launched in July 1978 atop a Titan IIIE-Centaur rocket and enter orbit round Mercury in may additionally 1980 with an orbital lifetime of four months. The spacecraft would have had an injected mass of three,one hundred twenty kilograms and an orbited mass of 775 kilograms, with the difference being the large volume of fuel required to convey the spacecraft into orbit around Mercury. The instrument mass would have been only 68.four kilograms.

The mission objectives would had been to map Mercury’s surface at 500-meter resolution, make huge measurements of the magnetospheric environment, examine the conception of gravitation the use of three different experiments, assess Mercury’s mass distribution, and assess the abundance of radioactive nuclides on the floor for composition studies. to accomplish this, the spacecraft could be geared up with two imaging cameras, two magnetometers, a 14-channel ultraviolet airglow sensor, a charged particle telescope, plasma science contraptions, an infrared radiometer, and a gamma-ray spectrometer.

The spacecraft would have been what JPL pointed out because the “Mercury Venus Mission ’seventy three spare,” in any other case ordinary because the backup to Mariner 10, outfitted with a new propulsion subsystem. Mariner 10 became a Venus and Mercury mission and the closing of the Mariner missions, youngsters the two Voyagers had been firstly given Mariner designations.

Mariner missions included backups in case of launch or spacecraft failures, which took place extra often than anybody liked. but Mariner 10 changed into now not deliberate to have a fully flight-certified spare. based on Bruce Murray and Eric Burgess of their 1977 e-book Flight to Mercury, at the beginning JPL planned on building an engineering spare that would not have all of the accessories required for flight. besides the fact that children, they saved enough cash on the primary spacecraft that they procured a full set of flight hardware for the backup, enabling it to fly if the primary spacecraft failed. When the mission was a success, the backup went into clean-room storage.

For the Mercury orbiting mission, the spacecraft would require new thermal coverage for its nearer proximity to the sun, an attitude control device developed for the Viking Orbiter, and hot-gas attitude control jets. The instrument suite could be a little bit diverse from Mariner 10. a large-attitude box of view television comparable to the one developed for Mariner 9, which become launched to Mars in 1971, would had been used and the ultraviolet occultation spectrometer deleted because it was unnecessary. The Viking Orbiter fuel tank would have been stretched about 0.6 meters. The spacecraft would trade out the 300-pounds-drive Viking engine, which turned into not sufficient to cope with slowing down the spacecraft so deep within the sun’s gravity smartly, and instead use a 900-pounds-drive response manage thruster engine developed for the area Shuttle.

The spacecraft would have been launched atop the strongest American rocket then in provider. it could conduct two swingbys of Venus a yr apart and would then be inserted into a 24-hour elliptical orbit inclined 70 degrees, with the northern-hemisphere periapsis at 500 kilometers altitude however its apoapsis a good deal farther out. This orbit would have allowed the spacecraft to map Mercury’s floor, gravitational field, and magnetosphere right through its brief lifetime in orbit. The final orbit inclination would had been chosen through a science steering group, but would probably be between one hundred ten and 135 levels. Getting an orbit that went over Mercury’s poles changed into important for several motives, including that it enabled the spacecraft to cover greater of the floor.

The document protected a desk that indicated that a Mercury orbiter changed into part of its “counseled application,” however a Mercury orbiting mission became not explicitly known as out within the text of the file.

The proposed trajectory meant a slow transit time to Mercury, nevertheless it resulted within the lowest retro speed that JPL’s trajectory specialists could achieve. That became the largest challenge for any Mercury orbiter: launching from Earth in opposition t the solar became almost launching downhill, requiring a lot of gas to slow all the way down to enter Mercury’s orbit instead of shoot past it and fritter away.

In 1975, the country wide analysis Council’s space Science Board introduced the consequences of its large overview of feasible actions within the area sciences. complex’s findings about photo voltaic gadget exploration have been included into the SSB’s document “alternatives and choices in space Science.” The basic suggestion for planetary science for NASA turned into to pursue a mission to come a pattern from the Martian surface—anything that remains an unachieved proper precedence for the planetary science community greater than forty years later. different top priorities have been to pursue outer planets research. The report did address the internal planets and the Moon, however these were clearly lessen priorities. regarding Mercury the document blanketed a table that indicated that a Mercury orbiter changed into a part of its “informed application,” but a Mercury orbiting mission became not explicitly called out in the text of the report.

Slowing down

In spring 1976, NASA Headquarters commissioned a “Mercury Orbiter Transport look at” from Science applications integrated that changed into presented to NASA in January 1977. The analyze was supposed to “assist NASA planners to assess the trajectory/payload efficiency requirements of candidate flight modes in delivering spacecraft systems to orbit the planet Mercury.”

The analyze looked at three different flight modes, 15- and 21-kilowatt solar electric powered propulsion options, and a photo voltaic sail, and recognized a range of transit instances and payload hundreds for Mercury missions. The file’s authors’ basic conclusion changed into that all three alternatives had been preferable to a more straightforward “ballistic trajectory” to Mercury like that proposed in the prior JPL examine.

Three years after advanced’s document basically de-emphasised Mercury, in 1978, the complicated committee issued the record “approach for Exploration of the internal Planets.” The document outlined the scientific desires for the exploration of Mercury including mapping, at a decision of one hundred meters or more advantageous, the half of the planet’s surface that had now not already been imaged.

The report stated that “At current, the U.S. means is restricted to ballistic-type launches, and the opportunities for such launches to insert an accurately instrumented payload into a circular orbit of Mercury are precluded by one or more” constraints. These protected small injected payload mass, few launch home windows, lengthy flight instances, and the skill to obtain most effective incredibly elliptical orbits “which would severely degrade the decision and insurance of surface chemistry, surface imagery, and warmth-move experiments.” The file recommended ready unless a “low-thrust” propulsion system—i.e. an ion engine or electric powered propulsion gadget—grew to become accessible. but if one of these equipment grew to be accessible, the committee suggested that a Mercury mission be adopted late in the length 1977–1987, on condition that it did not “detrimentally have an effect on” the examine of Earth, Mars, and Venus.

despite the fact there is no direct documentation to indicate it, apparently complex became no longer impressed with the proposed orbital mission the usage of the Mariner 10 backup. devoid of excessive-level scientific help, the Mercury orbiter mission didn't get NASA approval. NASA had better priority science missions by way of the later Seventies, and planetary missions were already competing with astrophysics for funding. Of all of the possible pursuits within the solar gadget, Mercury became no longer at the desirable of the priority checklist for additional examine, even though it may well be completed with a spare spacecraft. quickly planetary science entered a length of stagnation in the Nineteen Eighties, what some mentioned as the “misplaced decade” when no new planetary missions have been launched. The Mariner 10 backup changed into taken out of clean room storage and donated to the Smithsonian. In 2013, it was ultimately put on screen within the museum’s “Time and Navigation” gallery in Washington, DC.

Orbital maneuvers in the light

For the next decade, planning for a Mercury orbiter become very nearly nonexistent. NASA’s planetary science program was focused upon different desires. at the time, NASA turned into making no growth with photo voltaic sails, and changed into unwilling to commit to solar electric propulsion. For Mercury advocates, there became little cause to hope for a probable mission. however the circumstance changed into about to trade.

Yen’s work energized people interested in extra exploration of Mercury, and soon new experiences of Mercury missions have been undertaken by various corporations.

In 1985, JPL orbital dynamics professional Chen-Wan Yen turned his consideration to Mercury. He crunched the numbers for a range of launch home windows and trajectories and proven that it turned into possible to launch a spacecraft toward Mercury and by doing diverse flybys of the planet, mixed with small propulsive maneuvers, put a relatively small spacecraft into orbit. however the flight instances had been particularly long, on the order of three to 5 years, the benefit of this method become that it became feasible to location a larger payload into Mercury orbit than outdated alternatives. Even better, these trajectories might use the comparatively cheap and venerable Delta II launch vehicle.

Yen’s work energized people interested in additional exploration of Mercury, and shortly new reviews of Mercury missions were undertaken by using various groups. In 1985, ESA carried out a preliminary Mercury orbiter examine. In 1990–1992, the Russian Academy of Sciences’ area science department carried out informal Mercury orbiter experiences. additionally starting in 1992, Japan’s ISAS science agency considered a Mercury orbiter as a candidate for its “Planet C” mission. evidently, activity in Mercury turned into heating up.

In 1988, Yen led a JPL examine of a Mercury orbiter mission design and, that same year, NASA’s area Physics and Planetary Exploration Divisions supported a joint effort led with the aid of the Goddard house Flight center that consisted of several workshops and reviews over the several years. In February 1991, NASA published the consequences of the Mercury Orbiter Science Working team. The group outlined the science desires for any new mission to Mercury. The neighborhood also defined a fundamental mission to Mercury.

Goddard’s Mercury Orbiter science working group changed into chaired by J.W. Belcher of MIT. The science pursuits protected both planetology and magnetospheric physics. The planetary objectives had been to study the thermal and geological evolution of Mercury’s indoors and surface, the origins of the photo voltaic system and formation procedures, and new constraints on planetary magnetic field dynamos. The physics aims had been to analyze how particles from the solar behaved on both the day facet and evening side of Mercury. different goals covered learning photo voltaic flare strategies producing neutron and gamma ray emissions, photo voltaic full of life particle acceleration, origins of the solar wind and interplanetary magnetic container, and coronal mass ejections and circulation structure in the inner solar gadget. An astrophysics purpose turned into to look at colossal growth in relativity parameters and the solar gravity box. to achieve these science desires, the mission would require two just about identical spacecraft launched on a single rocket.

The Goddard group got here up with a listing of strawman science gadgets including an energetic particle detector, speedy electron analyzer, fast ion analyzer, gamma/X-ray spectrometer, ion composition plasma analyzer, line-scan imaging, a magnetometer, and an optimized solar wind analyzer, radio and plasma wave analyzer, and a solar neutron analyzer.

The strawman spacecraft changed into an octagon with two small photo voltaic panels on each and every of four of its sides able to featuring 415 watts at Mercury. These panels might fold up to in part cover the spacecraft and control heating. The spacecraft would even be included by means of forty layers of thermal wrap and spin at 10 rpm, with the spin axis perpendicular to solar course so that no facet confronted the solar for long. The spacecraft dry mass could be 800 kilograms, with 1,600 kilograms of gas. this could effect in a complete of 5,000 kilograms injected mass—two spacecraft plus a 200-kilogram launch car adapter. This brought as much as a very heavy mission. by using comparison, every Viking orbiter and lander pair weighed 3,527 kilograms.

The Goddard mission would require a Titan IV Centaur with diverse gravity assists at Venus and Mercury. The flight time may well be no less than three years and a optimum of six depending upon what number of Mercury flybys have been required before orbital insertion. The mission would emphasize magnetosphere survey for the first two Mercury years and planetary imaging for the 2nd two. the two spacecraft would enter distinctive orbits, with one in a 200-kilometer 12-hour polar orbit and the second in a really free equatorial orbit, ultimately changed to a polar orbit akin to the different spacecraft. The mission assumed launch alternatives in 1997, 1999, 2002, 2004, 2005m and 2007.

The gigantic number of Mercury mission proposals confirmed not only the hobby in doing such a mission, but the largely-accredited perception that Yen’s calculations had confirmed that it changed into now possible with a Delta II-type spacecraft.

The Goddard examine was performed when NASA nevertheless conceived of planetary missions as enormous and finished, and the twin-spacecraft mission with a mass far improved than Viking changed into big even for the time. Titan IV Centaurs were high priced rockets, and there are stories that the Goddard group even regarded using a shuttle launch. the overall charge of the Mercury Orbiter mission became estimated at about $650 million, requiring a major dedication by using NASA. but there with no trouble turned into not satisfactory scientific or political help for this sort of mission in the early 1990s. happily, another option had emerged.

the discovery software

within the early Nineteen Nineties, NASA had started a brand new software of smaller planetary spacecraft named Discovery. To kick off the trouble, NASA invited mission proposals for a gathering held in September 1992 in San Juan Capistrano, California. a few groups proposed Mercury missions:

  • Robert in a position of Lawrence Livermore proposed a Mercury interior, floor and Environmental Mission thought.
  • Duane Muhleman of Caltech proposed replicate, the Mercury Imaging and Radar Ranging Orbital Reconnaissance spacecraft.
  • Albert Metzger of JPL proposed a Mercury Mapping Orbiter mission.
  • Robert Nelson of JPL proposed the Hermes world Orbiter.
  • Bruce expenses of NASA’s Goddard house Flight middle proposed Mallcu.
  • Jacob Trombka of NASA Goddard proposed a Mercury container and surface Dynamics mission.
  • Stan Peale of UC Santa Barbara proposed a Mercury Geophysics Mission.
  • C.T. Russell of UCLA proposed the Mercury Magnetic, Gravity and Atmospheres mission.
  • Paul Spudis of the Lunar and Planetary Institute proposed the Mercury Polar Flyby mission.
  • Of about 70 proposed Discovery missions submitted to the San Juan workshop, nine of them were for Mercury, demonstrating not best the activity in doing this sort of mission, but the broadly-authorised perception that Yen’s calculations had proven that it was now possible with a Delta II-type spacecraft.

    Bruce bills, who worked within the Geodynamics department of NASA’s Goddard area Flight core proposed a Mercury mission named Mallcu, the Aymara identify for the Andean Condor, mythic partner of the solar god. Mallcu would enter polar orbit around Mercury with the intention of identifying the planet’s figure and middle of mass, signify its tidal amplitudes and phases, quantify its volcanism, symbolize its tectonic history, examine its have an effect on cratering, estimate its inside density distribution, make clear the beginning and nature of its magnetic container, and determine Mercury’s surface reflectivity.

    Mallcu would elevate most effective just a few devices. The simple one would be an instrument comparable to the Mars Observer Laser Altimeter (or MOLA). The Mercury edition would be smaller to evade overheating of colossal aperture optics so close to the solar. different contraptions would consist of a magnetometer and a digital camera. Observations of the spacecraft’s orbit around Mercury would permit scientists to improve a gravity mannequin for the planet. Mallcu would have an ordinary thermal insurance policy system, deploying two large colorations, looking form of like parasols, on both facet of the spacecraft. made from beta material, one would shelter from the solar, the different would protect from daylight reflected through Mercury.

    The Hermes global Orbiter mission would use a Delta II rocket to launch a 300-kilogram three-axis-stabilized spacecraft based mostly upon TRW’s Eagle spacecraft that the company turned into presenting for several Air force low Earth orbit missions. The spacecraft would enter a 12-hour polar orbit round Mercury with a low aspect of 200 kilometers and a high of 15,000 kilometers. The spacecraft would use a coloration and passive radiation to dwell cool. Hermes would elevate a visible camera, laser, laser detector unit, UV spectrometer and magnetometer. It had an estimated cost of $146 million.

    Duane Muhleman of Caltech proposed a spacecraft that, like Hermes, used TRW’s Eagle satellite bus. The idea became referred to as reflect, the Mercury Imaging and Radar Ranging Orbital Reconnaissance spacecraft. Jacob Trombka of NASA Goddard proposed a scaled-down version of Goddard’s Mercury Orbiter mission. The Mercury box and surface Dynamics mission would have used just one spacecraft as an alternative of two, and launched on a Delta II rocket, but other details are unavailable.

    Paul Spudis of the Lunar and Planetary Institute proposed a Mercury Polar Flyby mission that could fly past the planet two or thrice, about each six months, making observations of its poles, which were suspected of containing water ice. The primary science questions had been to examine if the polar caps are composed of water ice and to measure the temperature, extent, and purity of the polar ice. The spacecraft would also are seeking for to reply the geology of Mercury. The minimal requirement become for one polar pass and one equatorial circulate. The spacecraft would have a dry mass of 375 kilograms and an injected mass of 880 kilograms. It too would use a Delta launch automobile.

    despite the renewed pastime in Mercury, it nevertheless took decades for a mission to be proposed, chosen, and launched.

    Spudis’ spacecraft would be three-axis stabilized and consist of articulated solar arrays, a modular development with eight avionics bays, a gamma-ray spectrometer growth, and a rigidly mounted pre-deployed colour. according to Spudis, these design features had been proven on Mariner 10. The gadgets would include a neutron/gamma ray spectrometer, a thermal emission spectrometer, a narrow-attitude digital camera, and a radar sounder-scatterometer. The intention become to build the mission for $a hundred and forty million.

    MESSENGER launch

    Launch of the MESSENGER spacecraft in 2004. The growth in trajectory alternatives for Mercury made it possible to launch a spacecraft on a Delta II rocket and still region a considerable science payload in Mercury orbit. (credit score: NASA)

    Discovery to Mercury

    despite the renewed interest in Mercury sparked by means of Chen-Wan Yen’s 1985 trajectory calculations, and regardless of the numerous Mercury mission experiences of the late Nineteen Eighties and early Nineteen Nineties, it nonetheless took decades for a mission to be proposed, chosen, and launched.

    In 1996, NASA held a Discovery mission competition. one of the vital rivals became the Mercury surface, area environment, Geochemistry and Ranging mission, in any other case referred to as MESSENGER. In October 1997, NASA selected the Genesis and CONTOUR missions, but not MESSENGER. CONTOUR later suffered an in-flight failure, however Genesis became a hit in returning cometary dirt samples to Earth. In 1998, the agency held one more Discovery competition, and MESSENGER competed again. In July 1999, NASA chosen Deep have an impact on and MESSENGER as its next two Discovery missions. each missions had a price cap of $300 million and late 2004 launch dates.

    MESSENGER reached Mercury orbit in 2011, and for the subsequent a couple of years it greatly studied the planet, featuring statistics that is still being analyzed. The applied Physics Laboratory developed MESSENGER and fitted it with a heat preserve that kept it cool right through its mission—and also gave APL enough experience to later construct the Parker solar Probe, in order to function in an even greater hellish ambiance. In 2015, its gas depleted, MESSENGER crashed into Mercury’s floor.

    MESSENGER’s design, and its science, helped inform the development of the BepiColombo mission, to be able to conduct a an awful lot greater wide look at of Mercury. Assuming that each one goes to plot, BepiColombo will quickly beginning its event to Mercury, and when it reaches orbit in 2025, it might be partially as a result of the calculations of a JPL scientist 40 years earlier.

    word: we're briefly moderating all feedback subcommitted to deal with a surge in unsolicited mail.


    NASA solar Probe Flies with the aid of Venus on Its option to 'contact' the sun | killexams.com Real Questions and Pass4sure dumps

    A NASA solar-researching spacecraft's first Venus flyby is within the books.

    The company's Parker photo voltaic Probe zoomed inside 1,500 miles (2,400 kilometers) of Venus as deliberate this morning (Oct. 3), getting an orbit-sculpting gravity assist, NASA officials stated.

    The spacecraft hence continues to be on direction for its first shut come across with the sun, which is scheduled to take location from Oct. 31 through Nov. eleven. right through this 12-day stretch, the Parker solar Probe will accumulate a wealth of information about the solar's constitution, composition and activity.

    NASA's Parker photo voltaic Probe efficiently made its first flyby of Venus on Oct. 3, 2018 because the spacecraft makes its way towards the sun. The spacecraft may be the primary to fly through the solar's outer environment. Six greater Venus flybys are deliberate.

    credit: NASA/Johns Hopkins APL/Steve Gribben

    The spacecraft, which launched on Aug. 12, has many greater such encounters on tap — a complete of 24 over the next seven years. And there might be six more Venus flybys as neatly, with the intention to serve to shrink the Parker solar Probe's orbit, permitting it to get closer and closer to Earth's star over time.

    all through the final planned photo voltaic close strategy in 2025, for example, the spacecraft will zoom within three.83 million miles (6.sixteen million km) of the sun's surface. For viewpoint, the existing proximity record —which Parker will wreck late this month, incidentally — is 27 million miles (43 million km), set by the German-American Helios 2 mission in 1976.

    NASA’s Parker photo voltaic Probe will use seven Venus flybys over essentially seven years to steadily decrease its orbit around the sun, coming as shut as 3.eighty three million miles to the sun’s floor. the primary of those flybys happened on Oct. 3, 2018.

    credit: NASA/Johns Hopkins APL

    When all is asserted and carried out, the statistics gathered via the mission should greatly increase scientists' knowing of the sun and space climate, NASA officers have said. as an instance, the Parker photo voltaic Probe could assist resolve two lengthy-standing photo voltaic puzzles — why the solar's outer atmosphere, or corona, is so much hotter than the surface; and the way, precisely, the charged particles that make up the solar wind are accelerated to their brilliant speeds.

    Mike Wall's e-book about the search for alien life, "available," could be published on Nov. 13. observe him on Twitter @michaeldwall and Google+. observe us @Spacedotcom, fb or Google+. at the beginning published on space.com.


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    3D TSV Devices: Worldwide Market Analysis & Forecast 2018-2023 - ResearchAndMarkets.com | killexams.com real questions and Pass4sure dumps

    By Business Wire

    Article Rating:

    August 13, 2018 07:55 AM EDT  

    The "Global 3D TSV Devices Market - Growth, Trends and Forecast (2018 - 2023)" report has been added to ResearchAndMarkets.com's offering.

    The 3D TSV devices market is expected to register a CAGR of 6.88%, over the forecast period 2018-2023.

    Driven by the rising demand for novel, high-performance chip architectures featuring advantages such as greater performance, power utilization, and form factor features, 3D TSV technology is making healthy progress in the semiconductor industry.

    The development in the 3D TSV advanced wafer packaging technology market is presently fuelled by factors, such as strong outlook for the Information & Communication Technologies (ICT) sector, extension in communication services provider (CSP) operations, demand for advanced packaging, intensified activity in corporate data centers, and increasing propagation of cloud computing services.

    Key Highlights

  • Consumer Electronics to Witness Significant Growth Over the Forecast Period
  • China to Hold the Largest Market Share in Asia-Pacific
  • Adoption of Cloud-based Storage and Cloud Computing by Enterprises to Drive the Market Over the Forecast Period
  • Market Developments

  • May 2017 - Amkor Technology acquired Nanium SA, a manufacturer of WLFO technology. The acquisition is aimed at strengthening Amkor in the fast-growing market of wafer-level packaging for smartphones, tablets, and other applications.
  • Key Topics Covered

    1. Introduction

    2. Executive Summary

    3. Market Overview

    4. Market Dynamics

    5. Global 3D TSV Devices Market Segmentation

    6. Vendor Market Share Analysis

    7. Competitive Intelligence - Company Profiles

  • Amkor Technology, Inc. (US)
  • Globalfoundries (US)
  • Invensas Corporation (US)
  • Iwate Toshiba Electronics Co. Ltd. (Japan)
  • Micron Technology, Inc. (US)
  • Samsung Electronics Co. Ltd. (South Korea)
  • SK Hynix Inc. (South Korea)
  • Sony Corporation (Japan)
  • STATS ChipPAC Ltd. (Singapore)
  • Taiwan Semiconductor Manufacturing Company Limited (TSMC) (Taiwan)
  • Teledyne DALSA Inc. (Canada)
  • Tezzaron Semiconductor Corp. (US)
  • United Microelectronics Corporation (UMC) (Taiwan)
  • Xilinx Inc. (US)
  • 8. Investment Analysis

    9. Future of the Market

    For more information about this report visit https://www.researchandmarkets.com/research/nbh28p/3d_tsv_devices?w=4

    Copyright © 2009 Business Wire. All rights reserved. Republication or redistribution of Business Wire content is expressly prohibited without the prior written consent of Business Wire. Business Wire shall not be liable for any errors or delays in the content, or for any actions taken in reliance thereon.

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    StartEngine Announces Third Summit with Keynote from Chris Cox, Former SEC Chairman | killexams.com real questions and Pass4sure dumps

    By Business Wire

    Article Rating:

    August 7, 2018 09:01 AM EDT  

    StartEngine Crowdfunding Inc. (https://www.startengine.com/) will host the StartEngine Summit on October 19th, 2018 in Los Angeles, CA. This is StartEngine’s third crypto conference that focuses on ICOs, the tokenization of securities and alternative assets, and the trading of those tokens on the secondary market. The theme of this fall’s summit is “Tokenize the World,” and the event will continue to explore where innovation and US regulation intersect.

    Today, StartEngine announces the keynote speaker for the upcoming event: former SEC Chairman Christopher Cox, currently a partner at global law firm Morgan, Lewis & Bockius. This is the first time an SEC Chairman has spoken at a crypto event on regulation and the future of blockchain technology, and Cox’s keynote will be for attendees only and not streamed online with the rest of the Summit.

    At StartEngine’s last Summit, held this past April 20th, over 1,000 entrepreneurs and crypto enthusiasts attended the day-long event, which included over 40 panelists, 7 keynotes, and 12 ICO pitches. Speakers included Vinny Lingham (Civic), Ryan Singer (Chia), David Moss (StrongBlock), Josh Stein (Harbor), investor Gil Penchina, and venture capitalist Mark Suster.

    “We are ushering in a new era for ICOs and trading platforms with a former SEC chairman offering an exclusive keynote for the first time,” said Howard Marks, co-founder and CEO of StartEngine. “We see the convergence of crypto and SEC regulation as the next evolution in the fast growing ICO and trading marketplaces. The goal of the StartEngine Summit is to educate the marketplace, bring industry leaders together, and build the future of finance.”

    StartEngine is a modern financial firm that helps companies raise capital through the sale of securities, utilizing exemptions from registration under the Securities Act of 1933. To date, StartEngine has helped more than 160 companies raise capital, and the platform is ushering in a new tokenized securities market in which companies can sell tokenized securities and investors can trade them all on one platform.

    The StartEngine Summit will be an all-day event on October 19th, taking place at the Fairmont Miramar Hotel & Bungalows. Panel topics include how to tokenize alternative assets like real estate and commodities, what are the values and pitfalls of stablecoins, how to respond to a regulatory inquiry, and more.

    For more information on the StartEngine Summit visit: https://www.startenginesummit.com.

    About StartEngine

    StartEngine is a leading security offering platform that tokenizes securities for more efficient issuance and trading. Utilizing its expertise in regulated exempt offerings under the Securities Act, StartEngine has helped more than 160 companies raise capital and has over 150,000 registered investors. Based in Los Angeles, the company was created in 2014 by Howard Marks, co-founder of Activision, and Ron Miller. StartEngine is committed to revolutionizing the ways companies raise capital and to helping entrepreneurs achieve their dreams. StartEngine Crowdfunding is a not a broker-dealer, funding portal or investment adviser. StartEngine Capital, LLC is a funding portal registered with the US Securities and Exchange Commission (SEC) and a member of the Financial Industry Regulatory Authority (FINRA). Learn more about StartEngine at www.startengine.com.

    Copyright © 2009 Business Wire. All rights reserved. Republication or redistribution of Business Wire content is expressly prohibited without the prior written consent of Business Wire. Business Wire shall not be liable for any errors or delays in the content, or for any actions taken in reliance thereon.

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    Oct. 13, 2018 11:30 PM EDT

    By Liz McMillan

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    Oct. 13, 2018 07:30 PM EDT

    By Pat Romanski

    Data center, on-premise, public-cloud, private-cloud, multi-cloud, hybrid-cloud, IoT, AI, edge, SaaS, PaaS... it's an availability, security, performance and integration nightmare even for the best of the best IT experts. Organizations realize the tremendous benefits of everything the digital transformation has to offer. Cloud adoption rates are increasing significantly, and IT budgets are morphing to follow suit. But distributing applications and infrastructure around increases risk, introdu...

    Oct. 13, 2018 03:00 PM EDT

     


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