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  • 1
    Publication Date: 2016-06-07
    Description: The Fast Auroral Snapshot (FAST) Explorer spacecraft is to study the physical processes that produce the aurora borealis and aurora australis. It is a unique plasma physics experiment that will take fundamental measurements of the magnetic and electrical fields. This investigation will add significantly to our understanding of the near-earth space environments and its effect. The FAST has a 1 year requirement and 3-year goal for its mission life in low earth orbit. The FAST power power system topology is a Direct Energy Transfer (DET) system based on the SAMPEX design. The FAST flight battery supplies power to the satellite during pre-launch operations, the launch phase, the eclipse periods for all mission phases, and when the load is about 50 watts.
    Keywords: Energy Production and Conversion
    Type: The 1996 NASA Aerospace Battery Workshop; 469-492; NASA-CP-3347
    Format: application/pdf
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  • 2
    Publication Date: 2019-07-13
    Description: The Goddard Modular Smallsat Architecture (GMSA) is developed at NASA Goddard Space Flight Center (GSFC) to address future reliability along with minimizing cost and schedule challenges for NASA Cubesat and Smallsat missions.
    Keywords: Space Radiation; Electronics and Electrical Engineering; Spacecraft Design, Testing and Performance
    Type: GSFC-E-DAA-TN34070 , Annual AIAA/USU Conference on Small Satellites; Aug 06, 2016 - Aug 11, 2016; Logan, UT; United States
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  • 3
    Publication Date: 2019-07-12
    Description: This NASA Aerospace Flight Battery Systems Working Group was chartered within the NASA Engineering and Safety Center (NESC). The Battery Working Group was tasked to complete tasks and to propose proactive work to address battery related, agency-wide issues on an annual basis. In its first year of operation, this proactive program addressed various aspects of the validation and verification of aerospace battery systems for NASA missions. Studies were performed, issues were discussed and in many cases, test programs were executed to generate recommendations and guidelines to reduce risk associated with various aspects of implementing battery technology in the aerospace industry. This document contains Part 3 - Volume II Appendices to Part 3 - Volume I.
    Keywords: Electronics and Electrical Engineering
    Type: NASA/TM-2010-216729/VOL2/PT3 , NESC-RP-08-75 , NESC-RP-06-069-1 , L-19893 , NF1676L-10887
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  • 4
    Publication Date: 2019-07-12
    Description: This NASA Aerospace Flight Battery Systems Working Group was chartered within the NASA Engineering and Safety Center (NESC). The Battery Working Group was tasked to complete tasks and to propose proactive work to address battery related, agency-wide issues on an annual basis. In its first year of operation, this proactive program addressed various aspects of the validation and verification of aerospace battery systems for NASA missions. Studies were performed, issues were discussed and in many cases, test programs were executed to generate recommendations and guidelines to reduce risk associated with various aspects of implementing battery technology in the aerospace industry. This document contains Part 2 - Volume I: Recommendations for Technical Requirements for Inclusion in Aerospace Battery Procurements of the program's operations.
    Keywords: Space Transportation and Safety
    Type: NASA/TM-2010-216728/VOL1/PT2 , NESC-RP-08-75 , NESC-RP-06--069-1 , L-19890 , NF1676L-10884
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  • 5
    Publication Date: 2019-07-12
    Description: This NASA Aerospace Flight Battery Systems Working Group was chartered within the NASA Engineering and Safety Center (NESC). The Battery Working Group was tasked to complete tasks and to propose proactive work to address battery related, agency-wide issues on an annual basis. In its first year of operation, this proactive program addressed various aspects of the validation and verification of aerospace battery systems for NASA missions. Studies were performed, issues were discussed and in many cases, test programs were executed to generate recommendations and guidelines to reduce risk associated with various aspects of implementing battery technology in the aerospace industry. This document contains Part 2 - Volume II Appendix A to Part 2 - Volume I.
    Keywords: Space Transportation and Safety
    Type: NASA/TM-2010-216728/VOL2/PT2 , NESC-RP-08-75 , NESC-RP-06-069 , L-19891 , NF1676L-10885
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  • 6
    Publication Date: 2019-07-12
    Description: This NASA Aerospace Flight Battery Systems Working Group was chartered within the NASA Engineering and Safety Center (NESC). The Battery Working Group was tasked to complete tasks and to propose proactive work to address battery related, agency-wide issues on an annual basis. In its first year of operation, this proactive program addressed various aspects of the validation and verification of aerospace battery systems for NASA missions. Studies were performed, issues were discussed and in many cases, test programs were executed to generate recommendations and guidelines to reduce risk associated with various aspects of implementing battery technology in the aerospace industry. This document contains Part 3 - Volume I: Wet Life of Nickel-Hydrogen (Ni-H2) Batteries of the program's operations.
    Keywords: Space Transportation and Safety
    Type: NASA/TM-2010-216729/VOL1/PT3 , NESC-RP-08-75 , NESC-RP-06-069-1 , L-19882 , NF1676L-10886
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