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BATTERY, RECHARGEABLE, NICKEL-CADMIUM, VENTED, AIRCRAFT, BB-716/A

contributor authorARMY - CR - US Army Communications Electronics Command
date accessioned2017-09-04T17:06:29Z
date available2017-09-04T17:06:29Z
date copyright35712
date issued1997
identifier otherYFIBEAAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=anid=470393FD081DAC426159DD6EFDEC014A/handle/yse/130059
description abstractThis specification is approved for use within CECOM, Department of the Army, and is available for use by all Departments and Agencies of the Department of Defense.
The requirements for acquiring the product described herein shall consist of this specification sheet and the issue of MIL-PRF-49450 listed in that issue of the Department of Defense Index of Specifications and Standards (DoDISS) specified in the solicitation. FIGURE 1.  Markings and dimensions of battery (top view). FIGURE 2.  Markings and dimensions of battery (front and side views). FIGURE 3.  Battery strap configuration. TABLE I. Referenced components listing for figure 3.
REF LTR                    Description           Part Numbers     Quantity ---------------------------------------------------------------------------------------      A          Connector, Strap                  M49450/1-1          14     B          Diode Assembly                    M49450/2             1     C          Thermoswitch Assembly 1/          M49450/5-1           2     D          Thermistor Assembly 1,2/          M49450/5-2           2     D1         Connector, Insulated Strap 3/     M49450/1-3           2     E          Connector, Strap                  M49450-1-2           2     F          Cell, Low Capacity                M49450/6             1     G          Cell                              M49450/7            19     H          Partition, Metal (Removable)           ----            1     I          #10-32 Hexagonal Head Screw       AN3C3A               2     J          Belleville Spring                 M49450/3             2     K          Thermistor Assembly 1,3/          M49450/5-3           2  NOTES:  1. Part of Harness Assembly 2. Only applicable to Method 1 Harness Configuration 3. Only applicable to Method 2 Harness Configuration

FIGURE 4.  Wiring schematic diagram for battery. FIGURE 5.  Harness configuration (method 1). FIGURE FIGURE 7.  Cover hold-down pad.
languageEnglish
titleMIL-PRF-49450/8Anum
titleBATTERY, RECHARGEABLE, NICKEL-CADMIUM, VENTED, AIRCRAFT, BB-716/Aen
typestandard
page8
statusActive
treeARMY - CR - US Army Communications Electronics Command:;1997
contenttypefulltext


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