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  • 1
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    In:  CASI
    Publication Date: 2020-01-23
    Description: The paper introduces the midpoint monitoring method for detecting cell voltage imbalance in a series string of 8 electrochemical cells. Monte Carlo analysis is performed for normal cell End of Discharge open and closed circuit voltage behavior to assess the extent to which derived guard band voltage limits will detect over discharged cells, provide false positive indication, or fail to detect over discharged cells. Forward work is proposed to refine the battery monitoring method for operational use in 28V lithium ion batteries.
    Keywords: Engineering (General)
    Type: JSC-E-DAA-TN75972 , NASA Aerospace Battery Workshop; Nov 19, 2019 - Nov 21, 2019; Huntsville, AL; United States
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  • 2
    Publication Date: 2020-01-23
    Description: Low power Stirling convertors are being developed at NASA Glenn Research Center to provide future small spacecraft with electrical power by converting heat from one or more Light Weight Radioisotope Heater Units (LWRHU). An initial design converts multiple watts of heat to one watt of electrical power output using a Stirling convertor. A variety of mission concepts have been studied by NASA and the U. S. Department of Energy that would utilize low power Radioisotope Power Systems (RPS) for probes, landers, rovers, and repeaters. These missions would contain science instruments distributed across planetary surfaces or near objects of interest where solar flux is insufficient for using solar cells. Landers could be used to provide data such as, radiation, temperature, pressure, seismic activity, and other surface measurements for planetary science and to inform future mission planners. The studies propose using fractional versions of the General Purpose Heat Source or multiple LWRHUs to heat power conversion technologies for science instruments and communication. Dynamic power systems are capable of higher conversion efficiencies, which could enable equal power using less fuel or more power using equal fuel, when compared to less efficient static power conversion technologies. Providing spacecraft with more power would decrease duty cycling of basic functions and, therefore, increase the quality and abundance of science data. Efforts to develop the concept have focused on maturation of a 1-We convertor and controller design and performance evaluation of an evacuated metal foil insulation. A proof-of-concept 1-We convertor, controller, and evacuated metal foil insulation package have been fabricated and are undergoing characterization testing. The current status, findings, and path forward for the effort are explained in this paper.
    Keywords: Engineering (General)
    Type: NASA/TM-2019-220316 , AIAA–2019–4065 , E-19731 , GRC-E-DAA-TN71841 , International Energy Conversion Engineering Conference; Aug 19, 2019 - Aug 22, 2019; Indianapolis, IN; United States
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  • 3
    Publication Date: 2020-01-18
    Description: Cryogenic propellant storage tank self-pressurization involves complex physical phenomena which are usually analytically modelled via complex multidimensional CFD codes. Unfortunately these codes, even when modelling axisymmetric domains, may takes weeks or longer to obtain transient pressure and temperature information for relatively short periods of time (several seconds to several hours). Propellant tank storage end-to-end mission simulations can last a duration of days to weeks to months. Multi-node modelling of propellant tanks is a viable alternative to traditional CFD modelling and presents the advantage of greatly reduced run times on the order of hours and days compared to the weeks or longer for CFD codes. A multi-node model represents the fluid within the storage tank, as well as the storage tank itself, as a fluid-thermal network. This type of setup is not necessarily geometrically based. This can be accomplished using a commercial generalized fluid-thermal network code, such as SINDA/FLUINT (SF). The advantage of using a fluid-thermal network code like SF lies in its extensive ability to model the external environment of the storage tank through the graphical user interface, Thermal Desktop (TD). The total heat load into the tank may be a function of heaters and a complex radiative environment as well. Thermal Desktop may be used to address the detailed radiative environment of the tank as well as building a geometrically accurate depiction of the storage tank itself.
    Keywords: Engineering (General)
    Type: GRC-E-DAA-TN72353 , Propulsion and Energy Forum; Aug 19, 2019 - Aug 22, 2019; Indianapolis, IN; United States
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  • 4
    Publication Date: 2020-01-14
    Description: No abstract available
    Keywords: Engineering (General)
    Type: JPL-CL-16-4241 , AIAA/AAS Astrodynamics Specialist Conference; Sep 12, 2016 - Sep 15, 2016; Long Beach, CA; United States
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  • 5
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    In:  Other Sources
    Publication Date: 2020-01-13
    Description: No abstract available
    Keywords: Engineering (General)
    Type: JPL-CL-16-3857 , Chadron State and Colorado State Student Presentation; Sep 01, 2016; Chaldron, NE; United States
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  • 6
    Publication Date: 2020-01-13
    Description: No abstract available
    Keywords: Engineering (General)
    Type: JPL-CL-16-3795 , ASA - HITRAN 2016; Aug 24, 2016 - Aug 26, 2016; Reims; United States
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  • 7
    Publication Date: 2020-01-08
    Description: No abstract available
    Keywords: Engineering (General)
    Type: JPL-CL-16-3626 , Applied Superconductivity Conference; Sep 04, 2016 - Sep 09, 2016; Denver, CO; United States
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  • 8
    Publication Date: 2020-01-07
    Description: No abstract available
    Keywords: Engineering (General)
    Type: JPL-CL-16-3458 , 2016 Electronics Technology Workshop (ETW); Jun 13, 2016 - Jun 16, 2016; Greenbelt, MD; United States
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  • 9
    Publication Date: 2020-01-07
    Description: No abstract available
    Keywords: Engineering (General)
    Type: JPL-CL-16-3267 , Rocky Mountain Conference on Magnetic Resonance; Jul 17, 2016 - Jul 21, 2019; Breckinridge, CO; United States
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  • 10
    Publication Date: 2020-01-07
    Description: The art of going from a notional vision of a system to a fully realizable design is called architecting. For an architecture to be realizable over its lifetime, it has to conform to many demands. Not only does it need to conform to the vision and its ultimate purpose, it needs to adhere to a world of requirements: affordability, reliability, legality, operability, simplicity, analyzability, testability, understandability, accessibility, manufacturability, and repairability, among many others. Ultimately, the architectures that hang together in many or all of these dimensions evoke a sense of elegance and beauty. Please join us as Frank Gehry and JPLers Rob Manning and Raul Polit-Casillas discuss examples of design and architecture, and the importance of a well-thought-out design.
    Keywords: Engineering (General)
    Type: JPL-CL-16-3138
    Format: text
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