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SAE - SAE AIR5561 - LITHIUM BATTERY POWERED PORTABLE ELECTRONIC DEVICES Organization: SAE
Date: 2013-10-01
Description: While work has been completed by other groups to develop standards for permanently installed, rechargeable lithium batteries, there is currently no aerospace standard for lithium battery powered portable electronic devices that are intended to be used in conjunction with flight operations.
SAE/TP - 2010-01-1770 - SYSTEM INTEGRATION OF A SAFE, HIGH POWER, LITHIUM ION MAIN BATTERY INTO A CIVIL AVIATION AIRCRAFT Organization: SAE/TP
Date: 2010-11-02
Description: The Cessna Citation CJ4, certified on March 12, 2010, is believed to be the first civil aircraft with a Lithium Ion main battery. The 26.4VDC, 44Ah Lithium Ion main battery weighs 54 lbs, a 35% weight saving over a Nickel-Cadmium battery.
SAE - SAE J2929 - SAFETY STANDARD FOR ELECTRIC AND HYBRID VEHICLE PROPULSION BATTERY SYSTEMS UTILIZING LITHIUM-BASED RECHARGEABLE CELLS Organization: SAE
Date: 2013-02-01
Description: Future Considerations As lithium-based rechargeable battery systems expand in their usage, new information related to safety will become available and additional international regulatory standards will be developed.
SAE - SAE J2950 - RECOMMENDED PRACTICES (RP) FOR SHIPPING TRANSPORT AND HANDLING OF AUTOMOTIVE-TYPE BATTERY SYSTEM - LITHIUM ION Organization: SAE
Date: 2012-02-01
Description: This RP aids in the identification, handling, and shipping of new and used un-installed lithium ion battery systems to and from specified locations. The generic term "battery system" shall be used to identify automotive-type and sized "traction" batteries when used as intended by the vehicle and battery system original equipment manufacturers (OEMs) for ground vehicles.
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.
SAE - SAE AIR1898 - MAINTENANCE OF BATTERIES AND BATTERY CHARGING AND SERVICING FACILITIES Organization: SAE
Date: 1998-12-01
Description: It does not address or pertain to automotive-type SLI (starting-lightingignition) batteries or any other types of batteries (such as nickel-cadmium, zinc, or lithium batteries) which may be on-board airport GSE for either motive power or auxiliary uses.
SAE - SAE J3071 - AUTOMOTIVE BATTERY RECYCLING IDENTIFICATION AND CROSS CONTAMINATION PREVENTION Organization: SAE
Date: 2016-04-01
Description: This SAE Battery Identification and Cross Contamination Prevention document is intended to provide information that may be applicable to all types of Rechargeable Energy Storage System (RESS) devices.
SAE/TP - 2010-01-1765 - SOH RECOGNITION OF LI-ION AVIATION BATTERIES VIA PASSIVE DIAGNOSTIC DEVICE Organization: SAE/TP
Date: 2010-11-02
Description: Nickel-Cadmium (NiCd), Valve Regulated Lead-Acid (VRLA), or Lithium-Ion (Li-ion) batteries are used to start engines, provide emergency back-up power, and assure ground power capability for maintenance and pre-flight checkout.
SAE - SAE J2990 - HYBRID AND EV FIRST AND SECOND RESPONDER RECOMMENDED PRACTICE Organization: SAE
Date: 2012-11-01
Description: Nickel metal hydride (NiMH) and lithium ion (Li-ion) batteries used for vehicle propulsion power are the assumed battery systems of this RP.
SAE/TP - 2009-01-3191 - ELECTROCHEMICAL TESTING AT SAFT TO SUPPORT HEALTH PROGNOSTICATION MANAGEMENT FOR AVIATION Organization: SAE/TP
Date: 2009-11-10
Description: Lithium ion batteries offer more power and longer cycle life than traditional technologies for many different applications.
SAE/TP - 2010-01-1799 - AIR-LAUNCHED EXPENDABLE SMALL UNMANNED AIRCRAFT SYSTEMS: INCREASING POWER AND EXTENDING ENDURANCE TO MEET OPERATIONAL NEEDS Organization: SAE/TP
Date: 2010-11-02
Description: Today, state of the art technology for Group 1 (0-20 lbs) and Group 2 SUAS (21 - 55 lbs), provides approximately 25 - 60 minutes of endurance with conventional lithium ion / lithium polymer batteries. However, to make air-launched expendable SUAVs viable for multiple mission scenarios, technology must be developed to allow for a mission endurance of a minimum of four hours.
SAE/TP - 2011-01-2627 - CURRENT AND NEXT-GENERATION ENERGY STORAGE DEVICES FOR MICRO VEHICLE APPLICATIONS Organization: SAE/TP
Date: 2011-10-18
Description: While most commercial and developmental vehicle platforms currently utilize commercial-off-the-shelf lithium polymer batteries for their energy storage needs, endurance times are limited to minutes and high discharge rates and dynamic electrical loads limit battery life.
MODUK - DEF STAN 00-970: PART 9 - DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT PART 9: REMOTELY PILOTED AIR SYSTEMS - ISSUE 13: 07/2015 Organization: MODUK
Date: 2015-07-13
Description: (3) WRT paragraph 1353: Sub-paragraphs (f) and (g) are specifically applicable to Nickel-Cadmium batteries, but may also be relevant to other battery technologies. Civil Certification Specifications do not apply these rules to Lead Acid batteries.
SAE/TP - 2010-01-1776 - INTEGRATION OF A MICROTUBULAR SOLID OXIDE FUEL CELL INTO A MINI-UAV: DESIGN AND SIMULATION OF POWER SYSTEM ARCHITECTURE Organization: SAE/TP
Date: 2010-11-02
Description: Mini UAVs in the <20kg category are widely operated by military and civilian organisations, usually for surveillance purposes, and many are electrically powered for low acoustic and infra-red observability. Despite recent improvements in Lithium Polymer battery technology, endurance is still usually limited to around 1 hour for fixed wing vehicles.

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