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MIL-PRF-29595A
BATTERIES AND CELLS, LITHIUM, RECHARGEABLE, AIRCRAFT, GENERAL SPECIFICATION FOR
Organization:
NAVY - AS - Naval Air Systems Command
Year: 2011
Abstract: This specification covers the general requirements for secondary (rechargeable) storage batteries of lithium electrochemistry including, but not limited to, lithium-ion, gel-polymer lithium-ion, and lithium polymer.Intended Use: The storage batteries covered by this specification are used in fixed-wing and rotary-wing military aircraft. The batteries are used for starting engines or auxiliary power units. They also provide electricity to support aircraft emergency loads, aeronautical and ground systems, and associated equipment, have non-removable covers, and are designed for maintenance-free operation (see 6.14.8). Some of the batteries may have a separate charger. Most of the batteries under this specification, however, are designed to be charged directly from the electrical bus via an integral charger that either is contained within the battery or is connected to the battery exterior. The batteries are also exposed for prolonged periods to extreme seagoing environments not encountered by civilian aircraft
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| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T18:35:34Z | |
| date available | 2017-09-04T18:35:34Z | |
| date copyright | 04/26/2011 | |
| date issued | 2011 | |
| identifier other | JJDQJEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho4703177D081D20686159DD6EFDEC9FCD/handle/yse/217618 | |
| description abstract | This specification covers the general requirements for secondary (rechargeable) storage batteries of lithium electrochemistry including, but not limited to, lithium-ion, gel-polymer lithium-ion, and lithium polymer.Intended Use: The storage batteries covered by this specification are used in fixed-wing and rotary-wing military aircraft. The batteries are used for starting engines or auxiliary power units. They also provide electricity to support aircraft emergency loads, aeronautical and ground systems, and associated equipment, have non-removable covers, and are designed for maintenance-free operation (see 6.14.8). Some of the batteries may have a separate charger. Most of the batteries under this specification, however, are designed to be charged directly from the electrical bus via an integral charger that either is contained within the battery or is connected to the battery exterior. The batteries are also exposed for prolonged periods to extreme seagoing environments not encountered by civilian aircraft | |
| language | English | |
| title | MIL-PRF-29595A | num |
| title | BATTERIES AND CELLS, LITHIUM, RECHARGEABLE, AIRCRAFT, GENERAL SPECIFICATION FOR | en |
| type | standard | |
| page | 48 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;2011 | |
| contenttype | fulltext |