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  • 1
    Electronic Resource
    Electronic Resource
    Bradford, West Yorkshire : Emerald
    Management of environmental quality 15 (2004), S. 622-628 
    ISSN: 1477-7835
    Source: Emerald Fulltext Archive Database 1994-2005
    Topics: Economics
    Notes: Environmental management systems (EMS) seek to make companies simultaneously more competitive and environmentally responsible. Improved environmental performance can be sought from the adaptation of techniques that emphasize reduction of waste and process/product redesign in the quest of reducing environmental impact. However, EMS lacks a framework to quantify improvements and much of the evidence of EMS's impact on financial performance is anecdotal. This lack of theoretical development has served to diminish corporate support, thus reducing the likelihood of EMS implementation due to a perceived cost disadvantage. This paper proposes, and tests, a framework to quantify EMS improvements to determine the impact of EMS strategies on financial performance. Our findings suggest that implementation of an EMS strategy does not negatively impact a firm's financial performance.
    Type of Medium: Electronic Resource
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  • 2
    Electronic Resource
    Electronic Resource
    New York, NY [u.a.] : Wiley-Blackwell
    Process Safety Progress 16 (1997), S. 72-77 
    ISSN: 1066-8527
    Keywords: Chemistry ; Chemical Engineering
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology , Process Engineering, Biotechnology, Nutrition Technology
    Notes: In 1970, the Alyeska Pipeline Service Company was formed to manage the design, costruction, operation and maintenance of the Trans-Alaska Pipeline System. The 800 mile long pipeline carries crude oil from Prudhoe Bay on the North Slope to Port Valdez on Prince William Sound. There are 11 pump stations located along the pipeline, each of which is equipped with a crude oil relief tank. Because of the potential flammable nature of the crude oil vapors being vented from the tanks, Alyeska wanted to determine the region surrounding the tanks within which the lower flammable limit (LFL) could be exceeded. Because numerical models cannot accurately model the flow near structures, especially for dense gases (as is the case here), wind tunnel modeling was conducted to provide more accurate distance to LFL estimates. The wind tunnel model simulations were also used to judge the effect of various modeling parameters (i.e., site specific configurations, release scenarios and meteorological conditions), and to assist in possible future refinements to numerical models. Field observations were also obtained at one of the pump stations for the purpose of validating the wind tunnel modeling. The project, wind tunnel scaling methods, experimental methods, concentration measurement results, distance to LFL estimates and comparison between the field and wind tunnel observations are described in this paper.
    Additional Material: 9 Ill.
    Type of Medium: Electronic Resource
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  • 3
  • 4
    Publication Date: 2020-11-12
    Description: Background The aim of this study was to investigate if choice over resistance training exercise order affects motor performance and psychological outcomes among elite youth hockey players. Methods Seventeen elite hockey players (male, n = 14; female, n = 3, age: 15.1 ± 1.1 years) participated in this study. In the first session, individual optimum power loads were calculated in the back squat, jump squat, bench press and bench throw exercises. Then, in four counterbalanced sessions, participants completed three sets of six repetitions in the same exercises loaded with their optimum power loads. In two sessions, athletes used a self-selected order of exercises, while in other two sessions the order was predetermined. Power outputs were estimated with a linear position transducer. Fatigue and enjoyment were measured during and after the sessions using standardized questionnaires. Repeated measures analyses of variance and a paired-sample t-test were used to compare the effects between conditions. Results We observed trivial to small differences between conditions in power outputs (p ≥ 0.07; ES ≤ 0.21), fatigue (p ≥ 0.42; ES ≤ 0.33) and enjoyment (p = 0.72; ES = 0.05). Conclusion Given the comparable effects between approaches, both can be used when coaching youth athletes. Self-selecting the order of exercises based on preferences is a feasible and practical coaching option when working with youth athletes.
    Electronic ISSN: 2167-8359
    Topics: Biology , Medicine
    Published by PeerJ
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  • 5
    Publication Date: 2019-07-12
    Description: A modified process yields lower levels of internal porosity for solder joints produced in reduced-gravity environments. The process incorporates both alternative materials and a modified procedure. The process provides the necessary cleaning action to enable effective bonding of the applied solder alloy with the materials to be joined. The modified process incorporates a commercially available liquid flux that is applied to the solder joint before heating with the soldering iron. It is subsequently heated with the soldering iron to activate the cleaning action of the flux and to evaporate most of the flux, followed by application of solder alloy in the form of commercially available solid solder wire (containing no flux). Continued heating ensures adequate flow of the solder alloy around and onto the materials to be joined. The final step is withdrawal of the soldering iron to allow alloy solidification and cooling of the solder joint.
    Keywords: Space Processing
    Type: MSC-24023-1 , NASA Tech Briefs, February 2012; 14
    Format: application/pdf
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  • 6
    Publication Date: 2019-07-19
    Description: The International Space Station (ISS) enables the study of supportability issues associated with long-duration human spaceflight. The ISS is a large, complex spacecraft that must be maintained by its crew. In contrast to the Space Shuttle Orbiter vehicle, but similar to spacecraft that will be component elements of future missions beyond low-Earth orbit, ISS does not return to the ground for servicing and provisioning of spares is severely constrained by transportation limits. Although significant technical support is provided by ground personnel, all hands-on maintenance tasks are performed by the crew. It is expected that future missions to distant destinations will be further limited by lack of resupply opportunities and will, eventually, become largely independent of ground support. ISS provides an opportunity to begin learning lessons that will enable future missions to be successful. Data accumulated over the first several years of ISS operations have been analyzed to gain a better understanding of maintenance-related workload. This analysis addresses both preventive and corrective maintenance and includes all U.S segment core systems. Systems and tasks that are major contributors to workload are identified. As further experience accrues, lessons will be learned that will influence future system designs so that they require less maintenance and, when maintenance is required, it can be performed more efficiently. By heeding the lessons of ISS it will be possible to identify system designs that should be more robust and point towards advances in both technology and design that will offer the greatest return on investment.
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-CN-8091 , Space Technology and Applications International Forum 2004; Feb 08, 2004 - Feb 12, 2004; Albuquerque, NM; United States
    Format: application/pdf
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  • 7
    Publication Date: 2019-07-19
    Description: Future long-duration human exploration missions will be challenged by resupply limitations and mass and volume constraints. Consequently, it will be essential that the logistics footprint required to support these missions be minimized and that capabilities be provided to make them highly autonomous from a logistics perspective. Strategies to achieve these objectives include broad implementation of commonality and standardization at all hardware levels and across all systems, repair of failed hardware at the lowest possible hardware level, and manufacture of structural and mechanical replacement components as needed. Repair at the lowest hardware levels will require the availability of compact, portable systems for diagnosis of failures in electronic systems and verification of system functionality following repair. Rework systems will be required that enable the removal and replacement of microelectronic components with minimal human intervention to minimize skill requirements and training demand for crews. Materials used in the assembly of electronic systems (e.g. solders, fluxes, conformal coatings) must be compatible with the available repair methods and the spacecraft environment. Manufacturing of replacement parts for structural and mechanical applications will require additive manufacturing systems that can generate near-net-shape parts from the range of engineering alloys employed in the spacecraft structure and in the parts utilized in other surface systems. These additive manufacturing processes will need to be supported by real-time non-destructive evaluation during layer-additive processing for on-the-fly quality control. This will provide capabilities for quality control and may serve as an input for closed-loop process control. Additionally, non-destructive methods should be available for material property determination. These nondestructive evaluation processes should be incorporated with the additive manufacturing process - providing an in-process capability to ensure that material deposited during layer-additive processing meets required material property criteria.
    Keywords: Lunar and Planetary Science and Exploration
    Type: KSC-2007-180
    Format: application/pdf
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  • 8
    Publication Date: 2019-08-13
    Description: No abstract available
    Keywords: Avionics and Aircraft Instrumentation
    Type: KSC-2007-226 , NASA Exploration System Mission Directorate (ESMD) Technology Exchange Conference 2007; Nov 14, 2007 - Nov 15, 2007; Galveston, TX; United States
    Format: application/pdf
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  • 9
    Publication Date: 2019-07-13
    Description: This viewgraph presentation reviews some of the logistic issues that the Vision for Space Exploration will entail. There is a review of the vision and the timeline for the return to the moon that will lead to the first human exploration of Mars. The lessons learned from the International Space Station (ISS) and other such missions are also reviewed.
    Keywords: Lunar and Planetary Science and Exploration
    Type: Department of the Army Integrated Logistics Support (ILS) Conference; May 02, 2005 - May 05, 2005; Huntsville, AL; United States
    Format: application/pdf
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  • 10
    Publication Date: 2019-07-13
    Description: Future small and micro-missions, such as Mars Scouts and Deep Space probes, require a new look at highly integrated, re-configurable, low power avionics. This paper will present our plans for developing a scalable, configurable, and highly integrated 32-bit embedded platform capable of implementing computationally intensive signal processing and control algorithms in space flight instruments and systems. This platform is designed to service the need of both small and large spacecraft and planetary rovers that will operate within moderate radiation environments. Some of the key characteristics of this platform are its small size, low power, high performance, and flexibility. This estimated 10 fold reduction in both size and power over state-of-the-art processing platforms will enable this new product to act as the core of a low-cost mobility system for a wide range of missions.
    Type: AIAA Space 2004; Sep 28, 2004 - Sep 30, 2004; San Diego, CA; United States
    Format: text
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