1、INCH-POUND MIL-PRF-32271/15 9 June 2010 PERFORMANCE SPECIFICATION SHEET BATTERY, NON-RECHARGEABLE, LITHIUM This specification is approved for use by all Departments and Agencies of the Department of Defense. The requirements for acquiring the product herein shall consist of this specification sheet
2、and MIL-PRF-32271. FIGURE 1 M32271/15-12E Dimensions and marking locations FIGURE 1 NOTES: All dimensions are in inches Tolerance for all is 0.031 inches AMSC N/A FSC 6135 DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited Copyright Communications - Electronics Command
3、Provided by IHS under license with CRAINot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32271/15 123456Batt -Batt +DataClockFIGURE 2: Terminal marking detail 10%30%50%70%90%.140 MAX.400 .100.400 .100FIGURE 3: State of charge indicator detail FIGURE 3 NOTE: A
4、ll dimensions are in inches REQUIREMENTS (see 1.2 for Type, Class, and Features descriptions): Type I Class 2 Features E PIN M32271/15-12E Approved chemistry: Lithium manganese dioxide (Li/MnO2) Specification requirements: The following requirements of MIL-PRF-32271, identified therein as “when spec
5、ified”, are applicable as indicated below: 2 Copyright Communications - Electronics Command Provided by IHS under license with CRAINot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32271/15 Requirement Specification Reference Applicability Parallel cell arran
6、gements 3.4 No Connectors13.4.5 Yes Battery charger connection 3.4.5.1 No Connection integrity 3.4.5.2 No Terminal integrity 3.4.6 No Socket strength 3.4.6.1 No Terminal strength 3.4.6.2 No Complete discharge device 3.4.7 Yes State of charge device 3.4.8 Yes State of charge data output 3.4.8e Yes Ce
7、ll charging 3.5.3 Yes Nail penetration 3.5.4 Yes Cell series string short circuit 3.5.6 No Parallel string charge protection 3.5.6.1 No Charge protection 3.5.11 Yes Over-current protection 3.5.13.1 Yes Over-temperature protection 3.5.14 Yes Surface temperature 3.6h Yes Capacity tests LR and LRT No I
8、mmersion 3.7.8 No Watertight integrity13.7.9 Yes DO NOT CHARGE! marking 3.8.1.2b No Complete discharge device 3.8.4 Yes marking/label State of charge marking 3.8.5 Yes Dimensions, marking and configuration Battery Connector Glenair Part Number 807 198 07ZNU6 6DY Mating Connector Genair Part Number 8
9、07-162-06ZNU6-6PYB Battery Charger Connector Not Applicable Battery voltages (3.4.4 CS115; CS116; RE101; RE102; RS101; RS103. Watertight integrity (3.7.9) Delete in its entirety and replace with the following: 3.7.9 Watertight integrity. Batteries shall retain their watertight integrity and shall be
10、 capable of continuous use when immersed in water. During immersion, batteries shall be loaded and battery voltage shall remain above 10 volts. After immersion, battery weight gain shall be not greater than 0.1 gram. After the batteries have been tested as specified in 4.6.5.9 as modified herein, th
11、ey shall meet the visual, mechanical and battery voltage and capacity requirements. Verification Add the following to Table V - Group V Battery Inspections and Tests: Group No. Sample Size Inspection Requirement Paragraph Test Method Paragraph V C 3/ 5 Electromagnetic interference test 3.4.11 4.6.1.
12、11 Add the following note: 3/ The Group V C batteries will increase the size of the Group V from 46 to 51; Group V C batteries will be subject to all tests specified for the Group V batteries prior to separation into subgroups A, B, and C. Add the following new paragraph: 4.6.1.11 Electromagnetic in
13、terference test. The tests specified in MIL-STD-461 for the following parameters shall be performed on batteries connect to the Ground Soldier System: CS114, CS115, CS116, RE101, RE102, RS101, and RS103. Altitude (4.6.5.1) During exposure to low pressure, the open circuit voltage of the undischarged
14、 batteries shall be monitored and shall meet the requirement of 3.4.4.1. Vibration, Method 2 (4.6.5.3.2) Delete in its entirety and replace with the following: 4.6.5.3.2 Method 2. The batteries shall be subjected to Procedure I General Vibration IAW Test Method 514 of MIL-STD-810. The random vibrati
15、on levels shall comply with Category 24 Minimum Integrity Test requirements, and the test duration shall be no less than one hour for each of three orthogonal axes. Upon completion of the vibration test, battery voltage shall be tested in accordance with 4.6.1.5 for compliance to 3.4.4 and the batte
16、ries shall be examined for the visual and mechanical defects identified in Table XIV. Mechanical shock, Method 2 (4.6.5.4.2) Delete in its entirety and replace with the following: 4.6.5.4.2 Method 2. The batteries shall be subjected to the test of Method 516, Procedure I of MIL-STD-810. The peak saw
17、-tooth shock pulse of 40 gs and duration of 11 ms shall be used. Each battery shall be secured to the testing machine by means of a rigid mount. 6 Copyright Communications - Electronics Command Provided by IHS under license with CRAINot for ResaleNo reproduction or networking permitted without licen
18、se from IHS-,-,-MIL-PRF-32271/15 Each battery shall be subjected to a total of three shocks of equal magnitude. The shocks shall be applied in each of three mutually perpendicular directions for rectangular configurations or two for cylindrical configurations. Each shock shall be applied in a direct
19、ion normal to a face of the battery. The faces of the battery are identified by their position in relation to the face, which bears the electrical connector. Upon completion of the vibration test, battery voltage shall be tested in accordance with 4.6.1.5 for compliance to 3.4.4 and the batteries sh
20、all be examined for the visual and mechanical defects identified in Table XIV. Drop test (4.6.5.5) Delete the statement “Drop each battery once from a height of 30 2 inches onto a hard surface consisting of concrete” (lines 7 & 8), and replace with: “Drop each battery twice from a height not less th
21、an 90 inches onto three inches of -inch gravel backed by concrete.” All other test method requirements of 4.6.5.5 apply to the M32271/15-12E battery. Thermal shock (4.6.5.6) Delete references to “5 minutes” in steps 2 and 4 and replace with “1 minute.” All other test method requirements of 4.6.5.6 a
22、pply to the M32271/15-12E battery. Watertight integrity (4.6.5.9) Delete in its entirety along with all sub-paragraphs and replace with the following: 4.6.5.9 Watertight integrity. The batteries shall be subjected to Test Method 512, Procedure I of MIL-STD-810. Use salt water substitute prepared in
23、accordance with ASTM D-1141 for the test. Batteries shall be weighed in steps 1 and 7. Prior to the start of the test, the battery temperature shall be no less than 81F (27C) above the water temperature and the battery shall be at a full state of charge. Install a sealed mating connector to the batt
24、ery connector. The battery shall be completely immersed, in an upright orientation. The uppermost point of the battery shall be maintained at a depth not less than 1 meter beneath the surface of the water. Once immersed, the battery shall be loaded with a constant 18-watt load. In Step 6, the immers
25、ion time shall be 2 hours, and wiping or blotting shall be the only acceptable methods of drying. In Step 8, remove any small amounts of water by wiping or blotting. Upon completion of the test, remove the sealed mating connector. Upon completion of the watertight integrity test, battery voltage sha
26、ll be tested in accordance with 4.6.1.5 for compliance to 3.4.4 and the batteries shall be examined for the visual and mechanical defects identified in Table XIV. NOTES: (This section contains information of a general nature which may be helpful, but is not mandatory) Intended use: This battery is i
27、ntended for use in the Ground Soldier System. Please note that this battery must be electromagnetically compatible with the Ground Soldier System. Such compatibility is no guarantee of similar compatibility with any other system. Electromagnetic compatibility with any other system needs to be evalua
28、ted separately, and in the case of failure, either that system will need to adjust to this battery or another battery will need to be developed. 3Nominal ratings: The following are the nominal ratings for the battery described by this specification sheet. They are provided for information purposes.
29、3Capacity and energy delivered by a battery are significantly affected by usage conditions, such as temperature and loads applied. If you have any questions about use of this battery in a particular device or circumstance, please visit the following web site (contact info is posted): http:/www.cerde
30、c.army.mil/c2d/armypower. 7 Copyright Communications - Electronics Command Provided by IHS under license with CRAINot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32271/15 Battery PIN: M32271/15-12E (Li/MnO2) Overall Dimensions: 8.25 in. x 1.62 in. x 2.62 in
31、. MAX Weight: 1.75 lbs (739 grams) Voltage Range: 10.0-16.5 Nominal Capacity:(in ampere-hours) 10.5 Amp-hrs Nominal Energy:(in watt-hours) 132 Watt-hrs MAX rated power output: 36 watts MAX continuous load rating: 2.0 amperes MAX pulse load rating: 5.0 amperes Instantaneous trip rating: 10.0 amperes
32、Operating temperature range: -20 to 130F (-29 to 55C) Storage temperature range: -40 to 160F (-40 to 71C) MAX abusive temperature: (non-operating) 195F (91C) Other data: Military Type Designations. No version of this battery has been tested, evaluated, or used under any military type designations pr
33、ior to release of this specification sheet. Early versions of this battery were identified as “LM-145”. The type designation BA-5345/U has been approved for use with the M32271/15-12E battery. This battery is subject to the transportation requirements of 49 CFR 173.185. The battery has solid cathode
34、s and more than 2.0 grams of lithium content. See applicable Material Safety Data Sheet (MSDS) for the maximum lithium weight per cell and battery. It should be noted that all non-rechargeable lithium batteries are restricted from shipment as cargo aboard passenger aircraft within, entering, or leav
35、ing the US. This battery includes a complete discharge device in order to render the battery non-reactive after use. If the battery is damaged, or if the device does not operate as indicated by an amber or yellow light, the battery is considered reactive waste. This battery may be recycled after use
36、. Universal waste rules, where applicable, apply only when recycling is the chosen disposal method. The US Army CECOM Life Cycle Management Command (LCMC) publishes guidelines for the design of battery compartments for devices using the battery covered by this specification sheet: Technical Bulletin
37、 CECOM-TB-7. Please contact the CECOM LCMC Directorate for Safety at monm-amselsfsecconus.army.mil for further information. Navy safety tests of NAVSEA S9310-AQ-SAF-010 are required for this battery during first article testing. The test data provided from the testing will be used to evaluate applic
38、ations for specific using devices and Navy platforms. Devices using this battery will require US Navy Safety Approval prior to use by Department of Navy users unless such approval has already been granted. Please consult with NAVSEA Instruction 9310.1 for further information. 8 Copyright Communicati
39、ons - Electronics Command Provided by IHS under license with CRAINot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-32271/15 9 This battery is required to be electromagnetically compatible with the Ground Soldier System. Verification requirements include elect
40、romagnetic interference tests of MIL-STD-461 with the battery connected to the system. Battery vendors will need to coordinate with the Project Manager, Soldier Warrior (SWAR), in order to arrange to have their products evaluated in the system. Their address is: Project Manager, Soldier Warrior, ATT
41、N: SFAE-SDR-SWAR, 10125 Kingman Road, Building 317, Fort Belvoir, VA 22060-5820. Custodians: Preparing activity: Army CR Army CR Navy SH (Project Number 6135-2010-029) Air Force 99 DLA CC Review activities: Navy AS, MC Air Force 71 NOTE: The activities listed above were interested in this document a
42、s of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at https:/assist.daps.dla.mil or https:/assist.daps.dla.mil/quicksearch/. Copyright Communications - Electronics Command Provided by IHS under license with CRAINot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
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