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  • 1
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-07-13
    Description: The primary technical objective of this project is to undertake comprehensive testing to generate information on failure modes/criteria to better understand the reliability of: (1) Packages (e.g., Thin Small Outline Package [TSOP], Ball Grid Array [BGA], Plastic Dual In-line Package [PDIP]) assembled and reworked with lead-free alloys, (2) Packages (e.g., TSOP, BGA, PDIP) assembled and reworked with mixed (lead/lead-free) alloys.
    Keywords: Electronics and Electrical Engineering
    Type: KSC-2009-167 , 2009 SMTA AIMS Harsh Environment Electronics Symposium; Oct 05, 2009 - Oct 06, 2009; San Diego, CA; United States
    Format: application/pdf
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  • 2
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-07-13
    Description: In response to concerns about risks from lead-free induced faults to high reliability products, NASA has initiated a multi-year project to provide manufacturers and users with data to clarify the risks of lead-free materials in their products. The project will also be of interest to component manufacturers supplying to high reliability markets. The project was launched in November 2006. The primary technical objective of the project is to undertake comprehensive testing to generate information on failure modes/criteria to better understand the reliability of: - Packages (e.g., TSOP, BGA, PDIP) assembled and reworked with solder interconnects consisting of lead-free alloys - Packages (e.g., TSOP, BGA, PDIP) assembled and reworked with solder interconnects consisting of mixed alloys, lead component finish/lead-free solder and lead-free component finish/SnPb solder.
    Keywords: Electronics and Electrical Engineering
    Type: KSC-2009-207 , 2009 DMSMS and Standardization Conference; Sep 21, 2009 - Sep 24, 2009; Orlando, FL; Yemen, Republic of
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  • 3
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-07-13
    Description: The primary'technical objective of this project is to undertake comprehensive testing to generate information on failure modes/criteria to better understand the reliability of: Packages (e.g., Thin Small Outline Package [TSOP], Ball Grid Array [BGA], Plastic Dual In-line Package [PDIPD assembled and reworked with lead-free alloys Packages (e.g., TSOP, BGA, PDIP) assembled and reworked with mixed (lead/lead-free) alloys.
    Keywords: Electronics and Electrical Engineering
    Type: KSC-2008-045 , Cleaner, Sustainable Industrial Materials and Processes (C.S.I.M.P.) Workshop; Mar 17, 2008 - Mar 20, 2008; Coronado, CA; United States
    Format: application/pdf
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  • 4
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-07-13
    Description: The primary technical objective of the project is to undertake comprehensive testing to generate information on failure modes/criteria to better understand the reliability of: Packages (e.g., TSOP, BGA, PDIP) assembled and reworked with lead-free alloys Packages (e.g., TSOP, BGA, PDIP) assembled and reworked with mixed (lead/lead-free) alloys.
    Keywords: Electronics and Electrical Engineering
    Type: KSC-2007-080 , SMTA AIMS Harsh Environment Electronics Workshop; Jun 13, 2007 - Jun 14, 2007; Indianapolis, IN; United States
    Format: application/pdf
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  • 5
    Publication Date: 2019-07-12
    Description: National Aeronautics and Space Administration (NASA) Headquarters chartered the Technology Evaluation for Environmental Risk Mitigation Principal Center (TEERM) to coordinate agency activities affecting pollution prevention issues identified during system and component acquisition and sustainment processes. The primary objectives of NASA TEERM are to: Reduce or eliminate the use of hazardous materials or hazardous processes at manufacturing, remanufacturing, and sustainment locations. Avoid duplication of effort in actions required to reduce or eliminate hazardous materials through joint center cooperation and technology sharing. Corrosion is an extensive problem that affects the National Aeronautics and Space Administration (NASA) and the European Space Agency (ESA). The damaging effects of corrosion result in steep costs, asset downtime affecting mission readiness, and safety risks to personnel. Consequently, it is vital to reduce corrosion costs and risks in a sustainable manner. NASA and ESA have numerous structures and equipment that are fabricated from stainless steel. The standard practice for protection of stainless steel is a process called passivation. Passivation is defined by The American Heritage Dictionary of the English Language as to treat or coat (a metal) in order to reduce the chemical reactivity of its surface. Passivation works by forming a shielding outer (metal oxide) layer that reduces the impact of destructive environmental factors such as air or water. Consequently, this process necessitates a final product that is very clean and free of iron and other contaminants. Typical passivation procedures call for the use of nitric acid; however, there are a number of environmental, worker safety, and operational issues associated with its use. Citric acid is an alternative to nitric acid for the passivation of stainless steels. Citric acid offers a variety of benefits including increased safety for personnel, reduced environmental impact, and reduced operational cost. The primary objective of this effort is to qualify citric acid as an environmentally-preferable alternative to nitric acid for the passivation of stainless steel alloys. While citric acid use has become more prominent in industry, there is little evidence that citric acid is a technically sound passivation agent, especially for the unique and critical applications encountered by NASA and ESA.
    Keywords: Metals and Metallic Materials; Environment Pollution
    Type: KSC-E-DAA-TN35507
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  • 6
    Publication Date: 2019-07-12
    Description: Space Shuttle Program implemented tin whisker remediation strategy following discovery of tin whiskers in Orbiter hardware.
    Keywords: Electronics and Electrical Engineering
    Type: KSC-2009-097
    Format: application/pdf
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  • 7
    Publication Date: 2019-08-26
    Description: The use of conventional tin-lead (SnPb) in circuit board manufacturing is under ever-increasing political scrutiny due to increasing regulations concerning lead. The "Restriction of Hazardous Substances" (RoHS) directive enacted by the European Union (EU) and a pact between the United States National Electronics Manufacturing Initiative (NEMI), Europe's Soldertec at Tin Technology Ltd. and the Japan Electronics and Information Technology Industries Association (JEITA) are just two examples where worldwide legislative actions and partnerships/agreements are affecting the electronics industry. As a result, many global commercial-grade electronic component suppliers are initiating efforts to transition to lead-free (Pb-free) in order to retain their worldwide market. Pb-free components are likely to find their way into the inventory of aerospace or military assembly processes under current government acquisition reform initiatives. Inventories "contaminated" by Pb-free will result in increased risks associated with the manufacturing, product reliability, and subsequent repair of aerospace and military electronic systems. Although electronics for military and aerospace applications are not included in the RoHS legislation, engineers are beginning to find that the commercial industry's move towards RoHS compliance has affected their supply chain and changed their parts. Most parts suppliers plan to phase out their non-compliant, leaded production and many have already done so. As a result, the ability to find leaded components is getting harder and harder. Some buyers are now attempting to acquire the remaining SnPb inventory, if it's not already obsolete. Original Equipment Manufacturers (OEMs), depots, and support contractors have to be prepared to deal with an electronics supply chain that increasingly provides more and more parts with Pb-free finishes-some labeled no differently than their Pb counterparts-while at the same time providing the traditional Pb parts. The longer the transition period, the greater the likelihood of Pb-free parts inadvertently being mixed with Pb parts and ending up on what are supposed to be Pb systems. As a result, OEMs, depots, and support contractors need to take action now to either abate the influx of Pb-free parts, or accept it and deal with the likely interim consequences of reduced reliability due to a wide variety of matters, such as Pb contamination, high temperature incompatibility, and tin whiskering. Allowance of Pb-free components produces one of the greatest risks to the reliability of a weapon system. This is due to new and poorly understood failure mechanisms, as well as unknown long-term reliability. If the decision is made to consciously allow Pb-free solder and component finishes into SnPb electronics, additional effort (and cost) will be required to make the significant number of changes to drawings and task order procedures. This project is a follow-on effort to the Joint Council on Aging Aircraft/Joint Group on Pollution Prevention (JCAA/JG-PP) Pb-free Solder Project which was the first group to test the reliability of Pb-free solder joints against the requirements of the aerospace and military community.
    Keywords: Electronics and Electrical Engineering
    Type: KSC-2011-171R , KSC-2011-171 , 2011 SMTA International Conference; Oct 16, 2011 - Oct 20, 2011; Fort Worth, TX; United States
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  • 8
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-07-12
    Description: In response to concerns about risks from lead-free induced faults to high reliability products, NASA has initiated a multi-year project to provide manufacturers and users with data to clarify the risks of lead-free materials in their products. The project will also be of interest to component manufacturers supplying to high reliability markets. The project was launched in November 2006. The primary technical objective of the project is to undertake comprehensive testing to generate information on failure modes/criteria to better understand the reliability of: - Packages (e.g., TSOP, BOA, PDIP) assembled and reworked with solder interconnects consisting of lead-free alloys - Packages (e.g., TSOP, BOA, PDIP) assembled and reworked with solder interconnects consisting of mixed alloys, lead component finish/lead-free solder and lead-free component finish/SnPb solder.
    Keywords: Electronics and Electrical Engineering
    Type: KSC-2009-116
    Format: application/pdf
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  • 9
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-07-13
    Description: No abstract available
    Keywords: Electronics and Electrical Engineering
    Type: KSC-2009-042 , DoD Soldering Technologies Working Group (STWG); Apr 14, 2009 - Apr 15, 2009; Cocoa Beach, FL; United States
    Format: application/pdf
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  • 10
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-07-13
    Description: Original Equipment Manufacturers (OEMs), depots, and support contract ors have to be prepared to deal with an electronics supply chain that increasingly provides parts with lead-free finishes, some labeled no differently and intermingled with their SnPb counterparts. Allowance of lead-free components presents one of the greatest risks to the r eliability of military and aerospace electronics. The introduction of components with lead-free terminations, termination finishes, or cir cuit boards presents a host of concerns to customers, suppliers, and maintainers of aerospace and military electronic systems such as: 1. Electrical shorting due to tin whiskers 2. Incompatibility of lead-f ree processes and parameters (including higher melting points of lead -free alloys) with other materials in the system 3. Unknown material properties and incompatibilities that could reduce solder joint reli ability As the transition to lead-free becomes a certain reality for military and aerospace applications, it will be critical to fully un derstand the implications of reworking lead-free assemblies.
    Keywords: Electronics and Electrical Engineering
    Type: KSC-2010-122 , KSC-2009-311 , KSC-2010-163 , Surface Mount Technology Association International Conference; Oct 24, 2010 - Oct 28, 2010; Orlando, FL; United States|Pb-free Electronics Risk Management (PERM) Consortium; Jan 05, 2010 - Jan 07, 2010; Oak Ridge, TN; United States|DoD Soldering Technologies Working Group (STWG); Aug 24, 2010 - Aug 25, 2010; Columbus, OH; United States
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