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WILEY - LITHIUM ION BATTERIES - LITHIUM ION BATTERIES Organization: WILEY
Date: 1998-01-01
Description: Section 1.2 ("Design Considerations') introduces several definitions and the general considerations that make electrochemical cells using Li+ as the working ion the most promising elemental component for a secondary battery of high energy and power density.
SAE/TP - 2006-01-3023 - ADVANCED BIPOLAR LITHIUM ION BATTERY Organization: SAE/TP
Date: 2006-11-07
Description: This paper will present design data that will show the characteristics and the capabilities of the advanced bipolar lithium ion cells to meet the requirements for developing batteries which can enable batteries with a specific energy greater than 400 watt-hours per kilogram over a range of temperatures.
AIR FORCE - SMC-S-018 - LITHIUM-ION BATTERY FOR LAUNCH VEHICLE APPLICATIONS Organization: AIR FORCE
Date: 2008-06-13
Description: Compliance with this document is intended to assure a high-reliability product for achieving suitable battery performance during mission. Lithium-ion-based batteries are an evolving technology that has seen little use in launch vehicles to date.
NASA-LLIS-3516 - LESSONS LEARNED - LITHIUM-ION BATTERY FIRE Organization: NASA
Date: 2010-05-18
Description: Abstract: A lithium-ion battery undergoing characterization testing in a basement laboratory overheated, caught fire, and detonated, funneling toxic fumes into the two upper floors of the office building and forcing its evacuation for several days.
WSPC - LIT-ION BATT - LITHIUM-ION BATTERIES: SOLID-ELECTROLYTE INTERPHASE Organization: WSPC
Date: 2004-05-07
Description: This invaluable book focuses on the mechanisms of formation of a solid-electrolyte interphase (SEI) on the electrode surfaces of lithium-ion batteries. The SEI film is due to electrochemical reduction of species present in the electrolyte.
AIR FORCE - SMC-S-017 - LITHIUM-ION BATTERY FOR SPACECRAFT APPLICATIONS Organization: AIR FORCE
Date: 2008-06-13
Description: Application This report is intended for compliance in applicable military spacecraft acquisition and development to incorporate common requirements and practices necessary to assure successful lithium-ion battery operation during space missions. It is expected that battery piece parts, such as cell, cell-module, charge control electronics, bypass switch, heaters, temperature sensors, etc., are procured to lowerlevel qualification documents that define design, process, and quality controls, and qualification and acceptance test requirements.
SAE/TP - 2008-01-2895 - ADVANCED FEF3 CATHODE ENABLED LITHIUM-ION BATTERY Organization: SAE/TP
Date: 2008-11-11
Description: Although a number of factors within the battery cell contribute to this performance parameter, the most crucial one relates to how much energy can be stored in the positive and negative electrode materials of the lithium ion battery. Very little focus had been shown in the research of the electrochemistry of transition metal fluorides until Rutgers,, The State University of New Jersey began its investigation.
SAE/TP - 2008-01-2907 - A BATTERY ELECTRONICS UNIT (BEU) FOR BALANCING LITHIUM-ION BATTERIES Organization: SAE/TP
Date: 2008-11-11
Description: Lithium-ion batteries have become prominent in many applications, because of their high energy-to-weight ratio.
SAE/TP - 2008-01-2866 - HIGH POWER LITHIUM ION BATTERY FACILITATED BY AN ADVANCED CATHODE Organization: SAE/TP
Date: 2008-11-11
Description: In addition, the battery is capable of much higher specific power than typical lithium-ion batteries in use today.
ISO - FDIS 18243 - ELECTRICALLY PROPELLED MOPEDS AND MOTORCYCLES - TEST SPECIFICATION AND SAFETY REQUIREMENTS FOR LITHIUM-ION BATTERY SYSTEM Organization: ISO
Date: 2016-12-12
Description: This document specifies the test procedures for lithium-ion battery packs and systems to be used in electrically propelled mopeds and motorcycles.
SAE/TP - 2008-01-2865 - DESIGN CONSIDERATIONS WHEN DISPROPORTIONATE HEATING OF LITHIUM-ION BATTERY PACKS IS PRESENT Organization: SAE/TP
Date: 2008-11-11
Description: Follow-on efforts concentrated on battery pack data and were reported in 2007 through 2008. In these efforts lithium-ion cells and batteries (4P4S, 2P4S and 4S) were cycled at various conditions.
SAE/TP - 2010-01-1766 - FAULT MITIGATION AND CELL BALANCING OF HIGH POWER LITHIUM ION BATTERY PACKS Organization: SAE/TP
Date: 2010-11-02
Description: These same benefits have also led to widespread integration of lithium-ion products into the portable electronics markets. However, lithium-ion batteries carry their own disadvantages, including degradation at deep discharge, capacity loss at high temperatures, and susceptibility to catastrophic failure from venting (especially during charging), shorting, etc. that can have dire consequences on the platform.
ISO 17546 - SPACE SYSTEMS - LITHIUM ION BATTERY FOR SPACE VEHICLES - DESIGN AND VERIFICATION REQUIREMENTS - FIRST EDITION Organization: ISO
Date: 2016-03-01
Description: This International Standard specifies design and minimum verification requirements for lithium ion rechargeable (including lithium ion polymer) batteries for space vehicles.
DSF/PREN 62928 - RAILWAY APPLICATIONS – ROLLING STOCK EQUIPMENT – ONBOARD LITHIUM-ION TRACTION BATTERIES Organization: DS
Description: This standard specifies the lithium-ion battery technology but does not prevent the use of battery technologies other than lithium-ion technology for application as traction batteries.
SAE/TP - 2008-01-2885 - HIGH PERFORMANCE LITHIUM ION AIRCRAFT BATTERY FOR DOD PLATFORMS Organization: SAE/TP
Date: 2008-11-11
Description: Lithium-ion cells can be employed to produce a lithium-ion aircraft battery which will have significant advantages over the present nickel-cadmium and lead-acid aircraft batteries. The lithium-ion battery will have higher specific energy, increased energy density, improved cycle life, and lower maintenance requirements.
DSF/ISO/DIS 18300.2 - ELECTRICALLY PROPELLED ROAD VEHICLES -- SPECIFICATIONS FOR LITHIUM-ION BATTERY SYSTEMS COMBINED WITH LEAD ACID BATTERY OR CAPACITOR Organization: DS
Description: This standard specifies the lithium-ion battery systems combined with lead acid battery or electric double layer capacitor, to be used for automotive applications in voltage class A systems.
DSF/ISO/FDIS 18300 - ELECTRICALLY PROPELLED VEHICLES -- TEST SPECIFICATIONS FOR LITHIUM-ION BATTERY SYSTEMS COMBINED WITH LEAD ACID BATTERY OR CAPACITOR Organization: DS
Description: This standard specifies the lithium-ion battery systems combined with lead acid battery or electric double layer capacitor, to be used for automotive applications in voltage class A systems.
ISO - 18300 - ELECTRICALLY PROPELLED VEHICLES - TEST SPECIFICATIONS FOR LITHIUM-ION BATTERY SYSTEMS COMBINED WITH LEAD ACID BATTERY OR CAPACITOR - FIRST EDITION Organization: ISO
Date: 2016-11-15
Description: This document specifies the lithium-ion battery systems combined with lead acid battery or electric double layer capacitor to be used for automotive applications in voltage class A systems. document applies only to combinations of such electric energy storages that are integrated in a common housing.
DS/ISO 18300 - ELECTRICALLY PROPELLED VEHICLES – TEST SPECIFICATIONS FOR LITHIUM-ION BATTERY SYSTEMS COMBINED WITH LEAD ACID BATTERY OR CAPACITOR Organization: DS
Date: 2016-11-22
Description: ISO 18300:2016 specifies the lithium-ion battery systems combined with lead acid battery or electric double layer capacitor to be used for automotive applications in voltage class A systems. document applies only to combinations of such electric energy storages that are integrated in a common housing.
DIN 91252 - ELECTRICALLY PROPELLED ROAD VEHICLES - BATTERY SYSTEMS - DESIGN SPECIFICATIONS FOR LITHIUM-ION BATTERY CELLS; TEXT IN GERMAN AND ENGLISH Organization: DIN
Date: 2016-11-01
Description: The inner design, the cell chemistry and the electrical characteristics of the cells are not defined in this standard. NOTE 1 Tests for Lithium-ion based battery systems for electrically propelled road vehicles are specified in ISO 12405.

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