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BATTERY, RECHARGEABLE, NICKEL-CADMIUM, VENTED, AIRCRAFT, BB-432B/A

contributor authorARMY - CR - US Army Communications Electronics Command
date accessioned2017-09-04T17:02:04Z
date available2017-09-04T17:02:04Z
date copyright03/10/2000
date issued2000
identifier otherXSZFKAAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=anid=470393FD081DAC426159DD6EFDEC014A/handle/yse/125538
description abstractThis specification is approved for use by the USACECOM, Department of 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 and MIL-PRF-49450(CR)
Voltage. The voltage of the battery shall be 24 Vdc (nominal)
Capacity. The battery capacity shall be 10 ampere hours.
Weight. The weight of the battery shall be 34 pounds (Max)
Connector(J1). The main power connector shall be quick disconnect type that meets the dimensional and interface requirements of MS3509.
Connector(J2) The connector for the electrical harness shall be a 10 pin connector that meets the interface requirements of MS3474W12-10S.
Cells. The battery shall consist of 19 BB-599A/A cells in series.
languageEnglish
titleMIL-PRF-49450/9num
titleBATTERY, RECHARGEABLE, NICKEL-CADMIUM, VENTED, AIRCRAFT, BB-432B/Aen
typestandard
page6
statusActive
treeARMY - CR - US Army Communications Electronics Command:;2000
contenttypefulltext


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