MIL-PRF-XXXXX-1 - bulk charger - draft - 2024-09-03.pdf
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- Attached to
- RFI/Industry Day Universal Bulk Charger
- Solicitation number
- W91CRB-24-T-UBC
About this file
This document is a draft performance specification sheet for a Bulk Charger (PP-xxxx()/U) being developed by the U.S. Army. The charger is required to charge various military radio and wearable batteries, including the BB-2590/U, AN/PRC-148, AN/PRC-163, and Conformal Wearable Battery. The charger must meet specific requirements for physical characteristics, performance, electrical conditions, environmental conditions, safety, and reliability. It should be able to charge a variety of battery types in under 4 hours, have multiple USB ports, and operate in extreme temperatures and environmental conditions. The document also details system accessories like cables and power input options. This draft has not been approved for procurement, and the U.S. Army Contracting Command is conducting industry research on a Universal Bulk Charger through an RFI and Industry Day event.
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DO NOT USE FOR PROCUREMENT
NOTE: This draft, dated 3 September 2024, has not been approved for procurement.
DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.
9519951852 INCH-POUND
MIL-PRF-#####/1
3 September 2024
PERFORMANCE SPECIFICATION SHEET 1
CHARGER, BATTERY, PP-xxxx()/U 3
BULK CHARGER 4
This specification is approved for use by all 6
Departments and Agencies of the Department of Defense. 7
1 SCOPE 9
1.1 Scope. 12
The requirements for acquiring the product described herein shall consist of this specification sheet and 13
MIL-PRF-#####. 14
2 APPLICABLE DOCUMENTS 16
2.1 General. 19
The documents listed in this section are specified in sections 3, 4, or 5 of this specification. This section 20 does not include documents cited in other sections of this specification or recommended for additional 21 information or as examples. While every effort has been made to ensure the completeness of this list, 22 document users are cautioned that they must meet all specified requirements of documents cited in 23 sections 3, 4, or 5 of this specification, whether or not they are listed. 24
Comments, suggestions, or questions on this document should be emailed peosoldierstp@army.mil. Since 26 contact information can change, you may want to verify the currency of this address information using the 27
ASSIST Online database at https://assist.dla.mil. 28
NOTE: This draft, dated 3 September 2024 prepared by US
Army XXXXXX, has not been approved and is subject to modification. DO NOT USE PRIOR TO APPROVAL.
(Project 6130-xxxxx)
2.2 Government documents. 30
2.2.1 Specifications, standards, and handbooks. 32
As stated. 33
2.2.2 Other Government documents, drawings, and publications. 35
As stated. 36
2.3 Non-Government publications. 38
As stated. 39
2.4 Order of precedence. 40
As stated. 41
3 REQUIREMENTS 43
3.1 Specification sheets. 45
The individual item requirements shall be as specified herein and in accordance with MIL-PRF-XXXXX. 46
In the event of any conflict between the requirements of this specification sheet and MIL-PRF-XXXXX, 47 this specification sheet shall govern. 48
3.2 Inspections. 50
3.2.1 First article. 52
As stated. 53
3.2.2 Certification of conformity. 55
As stated. 56
TABLE I. Requirements requiring certification. 58
As stated.
3.3 Reserved 60
3.4 Physical characteristics. 62
3.4.1 Dimensions. 64
Add: The charger volume shall be not greater than 1.6 cubic feet when in transport configuration (see 65
3.4.7). No individual measurement (e.g. height, length or width) shall be greater than 30 inches. Verify in 66 accordance with 4.4.1. 67
TABLE II. System dimensions. 69
Dimension Charger in transport configuration
Width ≤ 30 inches
Length ≤ 18 inches
Height ≤ 12 inches
Volume ≤ 1.6 cu. ft.
3.4.2 Weight. 71
Add: The total weight of the charger, in fully operational configuration including the AC power cable, 72 shall weigh not greater than 35 pounds. Verify in accordance with 4.4.2. 73
3.4.3 Color. 75
Add: The charger and adapters shall be green (chip number 34088), tan (chip number 33446), or black 76
(chip number 37030) per SAE-AMS-STD-595. Surfaces shall have a dull lusterless finish. Cables may be 77 lusterless black (FED STD-595 color number 37038). Verify in accordance with 4.4.3. 78
3.4.4 Visual inspection. 80
As stated. 81
3.4.5 Stackable. 83
Add: When in transport configuration (see 3.4.7), the charger shall be stackable and stable up to 5 high 84 without damage. 85
3.4.5.1 Vertical alignment. 87
Add: The charger shall employ vertical alignment methods to prevent stacked chargers from shifting 88 beyond the footprint of the bottom charger and ensure aligned stacking. Verify in accordance with 4.4.5.1. 89
3.4.6 Handles. 91
As stated. 92
3.4.6.1 Handle strength. 94
As stated. 95
3.4.7 Transport configuration. 97
Add: The charger shall be able to be safely transported with all external components required for 98 operation, to include one full set of adapters and the AC cable. Any combination of adapters (see 3.5.1.3) 99 required to charge batteries listed in TABLE V shall be capable of being transported fully installed and 100 ready to operate. The charger and required components, in transport configuration, shall be capable of 101 being carried by one person with one hand. Verify in accordance with 4.4.7. 102
3.4.8 System connectors. 104
Any connector placed on the exterior of the case shall not protrude beyond the maximum dimensions of 105 the case. Any connector placed on the exterior of the case shall include some form of a tethered protection 106 from damage while not in use. 107
3.4.8.1 Non-proprietary connectors. 109
As stated. 110
3.4.8.2 DC input connector. 112
Add: The charger shall have one DC input connector. The DC input connector shall be clearly identified 113 as such. Verify in accordance with 4.4.8.2. 114
TABLE III. Reserved. 116
Reserved.
Reserved..
FIGURE 1. Reserved. 118
3.4.8.3 AC input connector. 120
Add: The charger shall have one AC input connector. The AC input connector shall be a 3-prong 121 receptacle compliant with IEC 60320 type C14. The AC input connector shall be capable of mating with 122 the AC Cable defined in 3.10.3.1. Verify in accordance with 4.4.8.3. 123
3.4.8.4 System modular connector. 125
N/A. 126
3.4.8.5 USB ports. 128
Modify: USB Type-C PD port minimum quantity shall be four. 129
3.4.8.6 Firmware upgrade port. 131
As stated. 132
3.4.9 Indicators. 134
As stated. 135
3.4.9.1 Blackout mode. 137
As stated. 138
3.4.9.2 Charger status indicators. 140
As stated. 141
TABLE IV. Battery charging indicators. 142
As stated.
Battery capacity. 144
As stated. 145
3.4.9.3 Digital display. 147
As stated. 148
3.4.10 Chemical agents. 150
As stated. 151
3.4.11 Marking. 153
As stated. 154
3.4.11.1 Nameplate label. 156
As stated. 157
Nameplate information. 159
As stated. 160
3.4.11.2 Firmware version label. 162
As stated. 163
3.4.11.3 Visibility of assembly markings. 165
As stated. 166
3.4.11.4 Battery interface nameplate labels. 168
As stated. 169
3.4.11.5 Battery interface markings. 171
As stated. 172
3.4.11.6 Power input/output label. 174
As stated. 175
3.5 Performance characteristics. 177
3.5.1 Battery charging. 179
As stated. 180
3.5.1.1 Battery types and charge times. 182
Add: 184
TABLE V. Basic configuration and charge times. 185
Battery [Minimum] number required
Energy (watt-hours) per battery
Max charge time (>90%
SOC)
(hours)
BB-2590/U 8 200 3
AN/PRC-148 Radio battery 16 52 2
AN/PRC-163 Radio battery 16 74 3
Conformal Wearable Battery (3.5/3.6) 16 148 3.5
Conformal Wearable Battery (3.6.2) 16 196 4.0
3.5.1.2 Charging protocols. 188
As stated. 189
System management bus (SMBus). 191
As stated. 192
Direct Query (DQ) protocol. 194
As stated. 195
Charging priority. 197
N/A. 198
Over-discharged batteries. 200
As stated. 201
3.5.1.3 Battery interface. 203
Replaceable battery interface. 205
Modify: The battery interfaces may utilize cables. 206
Charger connection. 208
As stated. 209
3.5.1.4 Charging with radios attached. 211
N/A. 212
3.5.1.5 Battery hot swap. 214
As stated. 215
Battery detect. 217
As stated. 218
3.5.1.6 STANREC 4819 compliance. 220
As stated. 221
3.5.2 USB ports. 223
3.5.2.1 USB Type-A receptacles. 225
As stated. 226
3.5.2.2 USB Type-C receptacles. 228
As stated. 229
3.5.3 Operability. 231
As stated. 232
3.5.3.1 Ease of systems operation. 234
As stated. 235
3.5.3.2 User interface. 237
As stated. 238
3.5.4 System characteristics. 240
3.5.4.1 On / off switch. 242
As stated. 243
3.5.4.2 Power on self-test. 245
As stated. 246
3.5.4.3 Power sharing. 248
N/A. 249
Power sharing hot swap. 251
N/A. 252
3.5.4.4 Upgradeability. 254
As stated. 255
New battery configurations. 257
As stated. 258
3.5.4.5 Cooling. 260
The charger may utilize a fan or fans for cooling. If fans are utilized for cooling, they shall be removable 261 and replaceable without tools or using a Phillips #1 or #2 screwdriver . Acoustic signature of fans shall be 262 limited to 35 dB at 1 meter. Verify in accordance with 4.5.4.5. 263
3.5.4.6 Vehicle mounting. 265
N/A. 266
N/A.
FIGURE 2. Vehicle mounting interfaces. 268
3.5.4.7 Ground post. 270
N/A. 271
3.5.5 Electrical characteristics. 273
3.5.5.1 Input voltage, AC. 275
Add: When operating under full load at 22°C±2°C, the charger shall utilize no less than 1,500 Volt-Amps 276
(VA) from a 120 VAC, 60 Hz source. 277
3.5.5.2 Input voltage, DC. 279
As stated. 280
3.5.5.3 Limited power sources. 282
The charger shall include user-selectable independent AC & DC power limits. Levels shall be 500 W, 750 283
W, 1,000 W, 1,250 W, Full Power, and Custom (user defined value). The default factory-programmed 284 limit shall be Full Power for AC and Full Power for DC. The power limit settings shall persist through a 285 charger power cycle. Verify in accordance with 4.5.5.3. 286
3.5.5.4 Automatic restart. 288
As stated. 289
3.5.5.5 Maximum power point tracking. 291
N/A. 292
3.5.5.6 Vehicle power. 294
N/A. 295
3.5.5.7 Reserved. 297
3.6 Electrical conditions. 299
3.6.1 Electromagnetic interference (EMI). 301
As stated. 302
3.6.1.1 CE102 (Conducted Emissions, Radio Frequency Potentials, Power Leads). 304
As stated. 305
3.6.1.2 CS101 (Conducted Susceptibility, Power Leads). 307
As stated. 308
3.6.1.3 CS114 (Conducted Susceptibility, Bulk Cable Injection). 310
As stated. 311
3.6.1.4 CS115 (Conducted Susceptibility, Bulk Cable Injection, Impulse Excitation). 313
As stated. 314
3.6.1.5 CS116 (Conducted Susceptibility, Dampened Sinusoidal Transients, Cables and Power 316
Leads). 317
As stated. 318
3.6.1.6 CS118 (Conducted Susceptibility, Personnel Borne Electrostatic Discharge). 320
As stated. 321
3.6.1.7 RE102 (Radiated Emissions, Electric Field). 323
As stated. 324
3.6.1.8 RS103 (Radiated Susceptibility, Electric Field). 326
As stated. 327
3.6.2 Reserved. 329
3.6.3 AC spikes and surges. 331
As stated. 332
3.6.4 DC spikes and surges. 334
As stated. 335
3.7 Environmental conditions. 337
As stated. 338
3.7.1 Temperature. 340
3.7.1.1 Operation. 342
Low temperature operation. 344
As stated. 345
High temperature operation. 347
As stated. 348
3.7.1.2 Storage. 350
Low temperature storage. 352
As stated. 353
High temperature storage. 355
As stated. 356
3.7.2 Humidity. 358
As stated. 359
3.7.3 Low pressure (altitude). 361
As stated. 362
3.7.4 Salt fog. 364
As stated. 365
3.7.5 Solar radiation. 367
As stated. 368
3.7.6 Temperature shock. 370
Replace: The charger, in transport configuration, shall withstand temperature shock in the range of -22°F 371
(-30°C) to +160°F (+71°C). When tested as specified in 4.7.6, the charger shall experience no deleterious 372 effects and shall meet full specification performance after testing. Verify in accordance with 4.7.6. 373
3.7.7 Transit. 375
As stated. 376
3.7.7.1 Loose cargo. 378
Add: This requirement applies to the charger in transport configuration. 379
3.7.7.2 Transit drop. 381
Add: This requirement applies to the charger in transport configuration. 382
3.7.8 Crash hazard shock. 384
N/A. 385
3.7.9 Vibration. 387
N/A. 388
3.7.10 Immersion. 390
Replace: The charger and accessories (as appropriate), in transport configuration, shall be capable of 391 being immersed and have drain holes (or similar features) as appropriate to minimize water retention. 392
After testing as specified in 4.7.10, the charger shall remain fully functional. Verify in accordance with 393
4.7.10. 394
3.7.11 Sand and dust. 396
As stated. 397
3.7.12 Rain. 399
As stated. 400
3.7.13 Fungus. 402
As stated. 403
3.7.14 Icing. 405
As stated. 406
3.7.15 Parachute landing fall impact. 408
N/A. 409
3.8 System safety. 411
3.8.1 General safety. 413
As stated. 414
3.8.1.1 Touch current (leakage current). 416
As stated. 417
3.8.1.2 Electric strength. 419
As stated. 420
3.8.1.3 Retained charge. 422
As stated. 423
3.8.2 Electrical shock. 425
As stated. 426
3.8.3 Short circuit. 428
As stated. 429
3.8.4 Over/under-temperature. 431
As stated. 432
3.8.5 Safety features. 434
3.8.5.1 Radioactive or hazardous materials. 436
As stated. 437
3.8.5.2 Non-rechargeable batteries. 439
As stated. 440
3.8.5.3 Surface temperature. 442
As stated. 443
3.8.5.4 Power outputs. 445
As stated. 446
3.9 Reliability. 448
As stated. 449
3.10 System accessories. 451
3.10.1 Solar panel. 453
N/A. 454
3.10.1.1 Solar panel characteristics. 456
N/A. 457
3.10.1.2 Power output at different solar angles. 459
N/A. 460
TABLE VI. Solar angle of incidence. 462
N/A
3.10.2 External AC to DC converter. 464
N/A. 465
3.10.2.1 Environmental requirements. 467
N/A. 468
3.10.3 Cables. 470
As stated. 471
3.10.3.1 AC input cable. 473
As stated. 474
3.10.3.2 DC power interface cable. 476
The DC power interface cable allows for an external DC power source to be connected to the charger. 477
The DC power interface cable shall have stranded copper based wire capable of carrying voltage and 478 current as specified in 3.5.5.2. The length shall be 6 feet +/- 3 inches. One end shall be capable of mating 479 with the DC input connector (see 3.4.8.2) on the charger. The other end shall be unterminated leads of 480 length 3 +/- 1 inches. Verify in accordance with 4.10.3.2. 481
N/A
FIGURE 3. Non-shrouded two wire “trailer hitch” connector. 483
3.10.3.3 DC extension cord cable (18 ft.). 485
N/A. 486
3.10.4 Additional DC inputs. 488
N/A. 489
N/A
FIGURE 4. Shrouded two wire “trailer hitch” connector. 491
3.10.4.1 NATO slave input power adapter. 493
The NATO slave plug shall be compatible with a Type I receptacle per NATO STANAG 4074 and be of 494 the minimum size and weight required to meet the power and environmental requirements of this 495 specification. 496
3.10.4.2 Alligator clips input power adapter. 498
N/A. 499
3.10.5 Hard cover. 501
The charger may have an integrated or removable hard cover which can be secured for transport 502 configuration (see 3.4.7). The charger and hard cover shall be designed to ensure that the cover does not 503 become a projectile. Verify in accordance with 4.10.5. 504
The system cover shall: 506
a. Meet the color requirements of the charger (see 3.4.3). 507
b. Have all latching mechanisms and connectors (e.g. snaps, rivets, etc) be lusterless. Hook and loop 508 straps (e.g. Velcro™) shall not be used. 509
c. Have a carrying handle capable of supporting not less than 60 pounds. 510
d. (if removable) Not require more than 15 seconds (for each action) to remove and replace from the 511 charger. 512
e. Be capable of storing the AC input cable and a full set of adapters required for charging batteries. 513
3.10.6 Soft cover. 515
N/A. 516
3.10.7 Transportation case. 518
N/A. 519
3.11 Repairability. 521
As stated. 522
4 VERIFICATION 524
4.1 Verifications of inspections. 526
As stated. 527
4.1.1 First article units. 529
The contractor will furnish first article units of the complete battery charger. The quantity of first article 530 units will be defined in the SoW. For all requirements where it states that verification or analysis is 531 required, the contractor shall detail the proposed testing and test protocols in the FAT Plan for 532 government review and acceptance. The presence of one or more defects shall be cause for rejection of 533
First Article and require all units to be tested for compliance with TABLE VIII. 534
4.1.2 First article inspection. 536
As stated. 537
4.1.3 Classification of verification. 539
As stated. 540
4.1.4 Methods of verification. 542
As stated. 543
TABLE VII. Verification methods table. 545
As stated.
4.1.5 Basis for verification. 547
The failure of any assembly, device, component, or test specimen to meet any of the verification criteria 548 shall be cause for rejection. The Government may use a waiver to accept products “as is” or terminate 549 verification requirements activities upon any failure to meet any of the requirements. The charger is 550 expected to meet all verifications as noted in TABLE VIII. 551
DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.
TABLE VIII. Performance Requirements - Verification Cross-Reference. 553
Section 4 Verification Method(s) of
Verification When Verified Sample/group
N /A
A n a ly si s
E x a m in a ti o
T es t
D em o n st ra ti
G v er n m en t
T es t*
P ro d u ct io n Q u a li fi ca ti
C n fo rm a n ce
A cc ep ta ce
R
P h y si ca l
(3 e a
R el ia b il it y e
T ra n si t D ro p e
E M
I/ E
M C e
T em p er a tu re e
E n v ir o n m en ta l
A e
E n v ir o n m en ta l
B e
B a tt er y c h a rg in g e
I n te rf a ce s (1 e
S a fe ty e
4.4 Physical characteristics. X
4.4.1 Dimensions. E X X ✔
4.4.2 Weight.visual E X ✔
4.4.3 Color. E X ✔
4.4.4 Visual inspection. E X X X ✔ ✔ ✔ ✔ ✔ ✔ ✔ ✔ ✔ ✔
4.4.5 Stackable. D X ✔
4.4.5.1 Vertical alignment. E X ✔
4.4.6 Handles. E X ✔
4.4.6.1 Handle strength. E X ✔
4.4.7 Transport configuration. D X ✔
4.4.8 System connectors. X
4.4.8.1 Non-proprietary connectors. A X
4.4.8.2 DC input connector. X
4.4.8.3 AC input connector. A X
4.4.8.4 System modular connector. X
4.4.8.5 USB ports. A X
4.4.8.6 Firmware upgrade port. A D X X ✔
4.4.9 Indicators. T X X ✔
4.4.9.1 Blackout mode. X
4.4.9.2 Charger status indicators. A T X ✔
4.4.9.2.1 Battery capacity. A X X
4.4.9.3 Digital display T X ✔
4.4.10 Chemical agents. T X ✔
4.4.11 Marking. E D X ✔
4.4.11.1 Nameplate label. E X X ✔
4.4.11.1.1 Nameplate information. E X X ✔
4.4.11.2 Firmware version label. E X ✔
4.4.11.3 Visibility of assembly markings. E X ✔
4.4.11.4 Battery interface nameplate labels. E X ✔
4.4.11.5 Battery interface markings. E X ✔
4.5 Performance characteristics. X
4.5.1 Battery charging. A T X X ✔
4.5.1.1 Battery types and charge times. A T X X ✔
4.5.1.2 Charging protocols. A X
4.5.1.2.1 System management bus (SMBus). A X
4.5.1.2.2 Direct Query (DQ) protocol. A X
4.5.1.2.3 Charging priority. X
4.5.1.2.4 Over-discharged batteries. T X ✔
4.5.1.3 Battery interface. X
4.5.1.3.1 Replaceable battery interface. A T X ✔
4.5.1.3.2 Charger connection. A T X ✔
4.5.1.4 Charging with radios attached. X
4.5.1.5 Battery hot swap. D X ✔
4.5.1.5.1 Battery detect. E X ✔
4.5.2 USB ports. T X ✔
4.5.3 Operability. D X ✔
4.5.3.1 Ease of systems operation. D X ✔
4.5.3.2 User interface. D X ✔
4.5.4 System characteristics. X
4.5.4.1 On / off switch. T X ✔
4.5.4.2 Power on self-test. T D X ✔
4.5.4.3 Power sharing. X
4.5.4.3.1 Power sharing hot swap. X
4.5.4.4 Upgradeability. A X
4.5.4.4.1 New battery configurations. A X
4.5.4.5 Cooling. E X ✔
4.5.4.6 Vehicle mounting. X
4.5.5 Electrical characteristics. X
4.5.5.1 Input voltage, AC. D X X ✔
4.5.5.2 Input voltage, DC. D X X ✔
4.5.5.3 Limited power sources. D X ✔
4.5.5.4 Automatic restart. D X ✔
4.5.5.5 Maximum power point tracking. X
4.5.5.6 Vehicle power. X
4.6 Electrical conditions. X
4.6.1 Electromagnetic interference (EMI). T X ✔
4.6.2 Reserved. T X
4.6.3 AC spikes and surges. T X ✔
4.6.4 DC spikes and surges. X ✔
4.7 Environmental conditions. X
4.7.1 Temperature. T X ✔ ✔
4.7.2 Humidity. T X ✔
4.7.3 Low pressure (altitude). T X ✔
4.7.4 Salt fog. T X ✔
4.7.5 Solar radiation. T X ✔
4.7.6 Temperature shock. T X ✔
4.7.7 Transit. X
4.7.7.1 Loose cargo. T X ✔
4.7.7.2 Transit drop. T X ✔
4.7.8 Crash hazard shock. X
4.7.9 Vibration. T X ✔
4.7.10 Immersion. T X ✔
4.7.11 Sand and dust. T X ✔
4.7.12 Rain. T X ✔
4.7.13 Fungus. A T X ✔
4.7.14 Icing. T X ✔
4.7.15 Parachute landing fall impact. X
4.8 System safety. X
4.8.1 General safety. E X X ✔ ✔
4.8.1.1 Touch current (leakage current). T X ✔
4.8.1.2 Electric strength. T X ✔
4.8.1.3 Retained charge. T X ✔
4.8.2 Electrical shock. A X
4.8.3 Short circuit. A X
4.8.4 Over/under-temperature. T X ✔
4.8.5 Safety features. X
4.8.5.1 Radioactive or hazardous materials. A X
4.8.5.2 Non-rechargeable batteries. D X ✔
4.8.5.3 Surface temperature. E X ✔
4.8.5.4 Power outputs. E X ✔
4.9 Reliability. T X ✔
4.10 System accessories. X
4.10.1 Solar panel. X
4.10.1.1 Solar panel characteristics. X
4.10.1.2 Power output at different solar angles. X
4.10.2 External AC to DC converter. X
4.10.2.1 Environmental requirements. X
4.10.3 Cables. T X ✔
4.10.3.1 AC input cable. E X ✔
4.10.3.2 DC power interface cable. E X ✔
4.10.3.3 DC extension cord cable (18 ft.). X
4.10.4 Additional DC inputs. X
4.10.4.1 NATO slave input power adapter. E X ✔
4.10.4.2 Alligator clips input power adapter. X
4.10.5 Hard cover. E X ✔
4.10.6 Soft cover. X
4.10.7 Transportation case. X
4.11 Repairability. A
* Government test does not negate the need for contractor production qualification testing. Government test is an independent verification performed in addition to 554 contractor production qualification testing. 555
TABLE IX. Applicable System Accessories for Test. 557
N/A
DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.
4.2 Conformance inspection. 560
As stated. 561
4.2.1 Nonconformance. 563
As stated. 564
4.2.2 Sampling and order of inspection. 566
As stated. 567
4.3 Common procedures. 569
As stated. 570
4.3.1 Basic operational test (BOT). 572
At ambient temperature charge twelve conformal wearable batteries (3.5/3.6), two BB-2590 batteries, and 573 two USB devices to not less than 90% state of charge. The charger shall meet the performance 574 requirements of 3.5.1 for these batteries. Verify the status indicators meet the requirements of 3.4.9 during 575 charge. 576
4.3.2 Basic functional test (BFT). 578
Connect the charger to its AC power source and allow the charger to perform a power on self-test (see 579
3.5.4.2). Connect an appropriate battery to each battery port and ensure charge is initiated. Connect a 580
USB compliant load to each USB charging receptacle (see 3.4.8.5) and verify that they meet the 581 requirements of 3.5.2. Connect a USB compliant computer to the USB data receptacle (3.4.8.6) and 582 ensure communications can be established. Verify operation of the Digital Display (3.4.9.3). Verify the 583 proper functionality of the blackout mode of 3.4.9.1. If accessories are being tested, perform the 584 appropriate test in paragraph 4.3.2.1 through 4.3.2.2. 585
4.3.2.1 BFT for DC power input accessories. 587
N/A. 588
4.3.2.2 BFT for additional battery interfaces. 590
Perform the BFT of 4.3.2 for each interface type installed. 591
4.4 Physical characteristics. 593
4.4.1 Dimensions. 595
Place the charger in transport configuration (see 3.4.7). Measure the charger including all protrusions to 596 the nearest tenth of an inch. System dimensions (width, length, and height) shall be from the largest flat 597 surface of each axis and shall not include any connector protrusions. Charger feet shall be considered in 598 the system height measurement. Verify that no dimension is greater than the value given in TABLE II. 599
Verify the total volume (L x W x H) is less than 1.6 cubic feet. 600
4.4.2 Weight. 602
Weigh the charger, not including battery interface adapters, AC and DC power cables, and verify that the 603 weight is not greater than 35 lbs. 604
4.4.3 Color. 606
Visually examine and verify that the color of the charger, cables, battery interfaces, and adapters is in 607 accordance with 3.4.3. 608
4.4.4 Visual inspection. 610
As stated. 611
4.4.5 Stackable. 613
The following test shall be performed. The charger shall meet the requirements of 3.4.5 and 3.4.5.1. 614
a. Configure five chargers in transportation configuration and stack them. 615
b. Apply increasing pressure to the front of the top charger until either 5 pounds of pressure is 616 applied or the charger has a lateral movement of 1 inch, whichever comes first. 617
c. Rapidly remove the pressure. 618
d. Verify that no charger falls and that no damage occurs. 619
e. Repeat steps b through d for each sides and the rear of the charger. 620
4.4.5.1 Vertical alignment. 622
Verify through examination that the charger, in transport configuration, has a method to align multiple 623 units when stacked on top of one another. 624
4.4.6 Handles. 626
As stated. 627
4.4.6.1 Handle strength. 629
As stated. 630
4.4.7 Transport configuration. 632
Verify through demonstration that the charger can be configured for transport with all external 633 components required for operation, to include one full set of adapters and the AC cable. Verify through 634 demonstration that the charger and required components, in transport configuration, can be carried by one 635 person with one hand. 636
4.4.8 System connectors. 638
N/A. 639
4.4.8.1 Non-proprietary connectors. 641
As stated. 642
4.4.8.2 DC input connector. 644
Verify through examination that the charger has one DC input connector and that the DC input is clearly 645 identified as such. 646
4.4.8.3 AC input connector. 648
Verify through examination that the charger includes an AC input using an IEC 60320 type C14 socket. 649
4.4.8.4 System modular connector. 651
N/A 652
4.4.8.5 USB ports. 654
As stated. 655
4.4.8.6 Firmware upgrade port. 657
As stated. 658
4.4.9 Indicators. 660
As stated. 661
4.4.9.1 Blackout mode. 663
As stated. 664
4.4.9.2 Charger status indicators. 666
As stated. 667
Battery capacity. 669
As stated. 670
4.4.9.3 Digital display 672
As stated. 673
4.4.10 Chemical agents. 675
As stated. 676
4.4.11 Marking. 678
As stated. 679
4.4.11.1 Nameplate label. 681
As stated. 682
Nameplate information. 684
As stated. 685
4.4.11.2 Firmware version label. 687
As stated. 688
4.4.11.3 Visibility of assembly markings. 690
As stated. 691
4.4.11.4 Battery interface nameplate labels. 693
As stated. 694
4.4.11.5 Battery interface markings. 696
As stated. 697
4.4.11.6 Battery interface markings. 699
As stated. 700
4.5 Performance characteristics. 702
4.5.1 Battery charging. 704
As stated. 705
4.5.1.1 Battery types and charge times. 707
As stated. 708
4.5.1.2 Charging protocols. 710
As stated. 711
System management bus (SMBus). 713
As stated. 714
Direct Query (DQ) protocol. 716
As stated. 717
Charging priority. 719
N/A. 720
Over-discharged batteries. 722
As stated. 723
4.5.1.3 Battery interface. 725
Replaceable battery interface. 727
As stated. 728
Charger connection. 730
As stated. 731
4.5.1.4 Charging with radios attached. 733
N/A. 734
4.5.1.5 Battery hot swap. 736
As stated. 737
Battery detect. 739
As stated. 740
4.5.1.6 STANREC 4819 compliance. 742
As stated. 743
4.5.2 USB ports. 745
4.5.2.1 USB Type-A receptacles. 747
As stated. 748
4.5.2.2 USB Type-C receptacles. 750
As stated. 751
4.5.3 Operability. 753
As stated. 754
4.5.3.1 Ease of systems operation. 756
As stated. 757
4.5.3.2 User interface. 759
As stated. 760
4.5.4 System characteristics. 762
4.5.4.1 On / off switch. 764
As stated. 765
4.5.4.2 Power on self-test. 767
As stated. 768
4.5.4.3 Power sharing. 770
N/A. 771
Power sharing hot swap. 773
N/A. 774
4.5.4.4 Upgradeability. 776
As stated. 777
New battery configurations. 779
As stated. 780
4.5.4.5 Cooling. 782
Visually inspect the charger to establish whether fan(s) are present. Verify through analysis (such as 783 system block diagrams or schematics) whether the charger utilizes fans for cooling. If so, verify through 784 demonstration that all fans can be removed and replaced without tools, or using a Phillips #1 or #2 785 screwdriver. At 22°C ±2°C, load the charger with a full set of discharged CWBs such that the charger 786 operates at maximum power. When all fans are active, verify that the acoustic level during operation is 787
<35 dB at a distance of 1 meter. 788
4.5.4.6 Vehicle mounting. 790
N/A. 791
4.5.4.7 Ground post. 793
N/A. 794
4.5.5 Electrical characteristics. 796
4.5.5.1 Input voltage, AC. 798
Add: Verify through test with a battery charging configuration causing the charger to operate at full load 799 at 22°C±2°C, the charger utilizes no less than 1,500 Volt-Amps (VA) from a 120 VAC, 60 Hz source. 800
TABLE X. Input voltage – frequency matrix. 802
As stated.
4.5.5.2 Input voltage, DC. 804
As stated. 805
4.5.5.3 Limited power sources. 807
Verify through examination that the charger includes user-selectable AC & DC power limiting with limits 808 specified in 3.5.5.3. Verify that the factory default limits are set to Full Power for AC and DC. Verify 809 through demonstration that the “custom” level can be changed. Verify through demonstration the charger 810 limits the AC power to each selected level by loading the charger with a full set of batteries and 811 monitoring the AC power source as the power limit setting is changed. Verify through demonstration the 812 charger limits the DC power to each selected level by loading the charger with a full set of batteries and 813 monitoring the DC power source as the power limit setting is changed. 814
4.5.5.4 Automatic restart. 817
As stated. 818
4.5.5.5 Maximum power point tracking. 820
N/A. 821
4.5.5.6 Vehicle power. 823
N/A. 824
4.5.5.7 Reserved.AC power limit negotiation (objective) 826
Verify though test that the charger can limit power draw in order to prevent overloading of a generator 827 supplying AC power. 828
4.6 Electrical conditions. 830
4.6.1 Electromagnetic interference (EMI). 832
As stated. 833
4.6.1.1 CE102 (Conducted Emissions, Radio Frequency Potentials, Power Leads). 835
As stated. 836
4.6.1.2 CS101 (Conducted Susceptibility, Power Leads). 838
As stated. 839
4.6.1.3 CS114 (Conducted Susceptibility, Bulk Cable Injection). 841
As stated. 842
4.6.1.4 CS115 (Conducted Susceptibility, Bulk Cable Injection, Impulse Excitation). 844
As stated. 845
4.6.1.5 CS116 (Conducted Susceptibility, Dampened Sinusoidal Transients, Cables and Power 847
Leads). 848
As stated. 849
4.6.1.6 CS118 (Conducted Susceptibility, Personnel Borne Electrostatic Discharge). 851
As stated. 852
TABLE XI. CS118 Discharge Table. 854
Discharge Location Type
1 Case (closed), Left Side Contact (±8 kV) & Air (±15 kV)
2 Case (closed), Right Side Contact (±8 kV) & Air (±15 kV)
3 Case (closed), Front Contact (±8 kV) & Air (±15 kV)
4 Case (closed), Back Contact (±8 kV) & Air (±15 kV)
5 Case (closed), Top Contact (±8 kV) & Air (±15 kV)
6 Case (closed), Bottom Contact (±8 kV) & Air (±15 kV)
7 Carrying handle Contact (±8 kV) & Air (±15 kV)
8 AC input socket, Ground Contact (±8 kV) & Air (±15 kV)
9 AC input socket, Line Contact (±8 kV) & Air (±15 kV)
10 AC input socket, Neutral Contact (±8 kV) & Air (±15 kV)
11 DC input connector, +VDC Contact (±8 kV) & Air (±15 kV)
12 DC input connector, Gnd Contact (±8 kV) & Air (±15 kV)
13 DC input connector, Shell Contact (±8 kV) & Air (±15 kV)
14 Digital display Contact (±8 kV) & Air (±15 kV)
15 Control button(s)/knob(s) Contact (±8 kV) & Air (±15 kV)
16 Charger contact(s) for battery interface (adapter) Contact (±8 kV) & Air (±15 kV)
17 Battery interface (adapter) contacts for batteries Contact (±8 kV) & Air (±15 kV)
18 USB Type-A socket(s), Shell Contact (±8 kV) & Air (±15 kV)
19 USB Type-C socket(s), Shell Contact (±8 kV) & Air (±15 kV)
4.6.1.7 RE102 (Radiated Emissions, Electric Field). 856
As stated. 857
4.6.1.8 RS103 (Radiated Susceptibility, Electric Field). 859
As stated. 860
4.6.2 Reserved. 862
4.6.3 AC spikes and surges. 864
As stated. 865
4.6.4 DC spikes and surges. 867
As stated. 868
4.7 Environmental conditions. 870
As stated. 871
4.7.1 Temperature. 873
4.7.1.1 Operation. 875
Low temperature operation. 877
As stated. 878
High temperature operation. 880
As stated. 881
4.7.1.2 Storage. 883
Low temperature storage. 885
As stated. 886
High temperature storage. 888
As stated. 889
4.7.2 Humidity. 891
As stated. 892
4.7.3 Low pressure (altitude). 894
As stated. 895
4.7.4 Salt fog. 897
As stated. 898
4.7.5 Solar radiation. 900
As stated. 901
4.7.6 Temperature shock. 903
Add: Procedure to be conducted with the charger in transport configuration. 904
4.7.7 Transit. 906
4.7.7.1 Loose cargo. 908
Place the charger in transport configuration and subject it to loose cargo testing in accordance with MIL-909
STD-810 Method 514 Procedure II for not less than 20 minutes in duration. During Step 4 conduct a BFT 910 as defined in 4.3.2 to determine operational status. Initial orientation shall be in the normal transportation 911 condition. Before and after testing, an operational checkout shall be performed and shall consist of the 912
BFT of 4.3.2. Verify that no damage occurs to the charger. 913
4.7.7.2 Transit drop. 915
The charger and accessories shall be tested in transport configuration. Verification shall be conducted in 916 accordance with Method 516, Procedure IV, of MIL-STD-810. Six samples shall be tested. Three of the 917 samples shall be tested at the minimum temperature of 3.7.1.2.1 and three of the samples shall be tested at 918 the maximum temperature of 3.7.1.2.2. All samples shall be dropped once on each face, edge, and corner. 919
All samples shall be soaked at the target temperature for a minimum of two hours, and all drops shall be 920 performed within thirty minutes of removal from the environmental chamber. After the completion of all 921 drops, verify that the charger remains functional by conducting a BFT as defined in 4.3.2. 922
4.7.8 Crash hazard shock. 924
N/A. 925
4.7.9 Vibration. 927
Verification test shall be conducted with the charger in transport configuration. Test in accordance with 928
MIL-STD-810 Method 514, Procedure I, (General vibration, operational service), Category 4 using the 929 composite wheeled vehicle vibration profile spectra (Figure 514.6C-3/Table 514.6C-VI). Conduct 930 operational checkout during Step 13 and as specified in the procedure using the BFT of 4.3.2. Verify that 931 no materials used to assemble the charger become dislodged during test. Repeat the verification for each 932 of the 3 major excitation axes. 933
TABLE XII. Battery configurations for vibration shock testing. 934
N/A
4.7.10 Immersion. 936
Add: Procedure to be conducted with the charger in transport configuration. 937
4.7.11 Sand and dust. 939
As stated. 940
4.7.12 Rain. 942
As stated. 943
4.7.13 Fungus. 945
As stated. 946
4.7.14 Icing. 948
As stated. 949
4.7.15 Parachute landing fall impact. 951
N/A. 952
4.8 System safety. 954
4.8.1 General safety. 956
As stated. 957
4.8.1.1 Touch current (leakage current). 959
As stated. 960
4.8.1.2 Electric strength. 962
As stated. 963
4.8.1.3 Retained charge. 965
As stated. 966
4.8.2 Electrical shock. 968
As stated. 969
4.8.3 Short circuit. 971
As stated. 972
4.8.4 Over/under-temperature. 974
As stated. 975
4.8.5 Safety features. 977
As stated. 978
4.8.5.1 Radioactive or hazardous materials. 980
As stated. 981
4.8.5.2 Non-rechargeable batteries. 983
As stated. 984
4.8.5.3 Surface temperature. 986
Load the charger with sixteen conformal wearable batteries and four USB PD 100W devices. Each battery 987 shall be less than 20% state of charge. The ambient temperature shall be 25°C +/- 3°C. Charge the 988 batteries and continually monitor the surface temperature of the charger during the charge to 95% or 989 higher state of charge. Verify that no surface temperature exceeds the touch temperature of MIL-STD-990
1472. 991
Repeat test at 45°C +/- 3°C. Store the charger and batteries at temperature for no less than four (4) hours 993 before starting charge. Charge the batteries and continually monitor the surface temperature of the 994 charger during the charge to 95% or higher state of charge. Verify that no surface temperature exceeds the 995 touch temperature of MIL-STD-1472. 996
4.8.5.4 Power outputs. 998
As stated. 999
4.9 Reliability. 1001
The following reliability test shall be performed on 3 charger systems to demonstrate requirements of 3.9. 1002
The systems shall accumulate a total cumulative hours of 895 operational hours with 3 maximum 1003 allowable failures. No one charger system shall accrue less than 220 hours. A failure is any hardware or 1004 firmware event that results in the inability of the charger to meet any specified performance requirements. 1005
Each charger shall be subjected to repeated 24-hour operational cycles, as described below, until the total 1007 cumulative hours are met. For all charging sessions, batteries under charge shall start from less than 10% 1008 state of charge. If necessary, to keep the charger in a charging state, charged batteries can be replaced 1009 with depleted batteries as needed for the duration of each charging session. For the purposes of this test, 1010 four PRC-148 batteries, two BB-2590 batteries, eight CWBs, two USB devices, and two USB PD 1011 devices, shall be referred to as a Battery Test Set. 1012
a. Place the charger in a test chamber capable of maintaining 45 ± 3°C. Connect the charger to a 120 1014
VAC source. 1015
b. At ambient room temperature (21 ± 3°C) load the charger with the Battery Test Set and begin 1016 charging. Charge batteries for not less than 4 hours. Remove batteries from charger, but leave the 1017 charger turned on. 1018
c. Set the chamber to 45 ± 3°C. Once the test temperature is reached allow the test items to stabilize 1019 for not less than four hours. 1020
d. Load the charger with the Battery Test Set and begin charging. Charge the batteries for not less 1021 than 4 hours. At the end of the charging session remove batteries from the charger. 1022
e. Place the charger in a vibration test chamber and subject the charger to Test Method Procedure I - 1023
General Vibration of MIL-STD-810. The vibration levels shall be as identified in Figure 514.6C-1024
3 - Category 4 - Composite Wheeled Vehicle Vibration Exposure. 1025
f. Connect the charger to a 120 VAC source. Load the charger with the Battery Test Set and start 1026 charging. Subject the charger with charging batteries to the vibration levels described by step e 1027 above for not less than 4 hours. This step shall be performed at ambient room temperature. 1028
g. Perform Basic Functional Test on the charger and batteries. Document any defects and anomalies. 1029
Remove batteries from charger, but leave the charger turned on. Allow the charger to soak at 1030 ambient room temperature (21 ± 3°C) for not less than 4 hours. 1031
h. Turn the charger off completely, and allow the charger to soak at ambient room temperature (21 ± 1032
3°C) for not less than 4 hours. 1033
i. Repeat cycle starting from step a until the chargers have accumulated the required operational 1034 hours. 1035
4.10 System accessories. 1037
As stated. 1038
4.10.1 Solar panel. 1040
N/A. 1041
4.10.1.1 Solar panel characteristics. 1043
N/A. 1044
4.10.1.2 Power output at different solar angles. 1046
N/A. 1047
4.10.2 External AC to DC converter. 1049
N/A. 1050
4.10.2.1 Environmental requirements. 1052
N/A. 1053
4.10.3 Cables. 1055
As stated. 1056
4.10.3.1 AC input cable. 1058
As stated. 1059
4.10.3.2 DC power interface cable. 1061
Verify through demonstration that the DC power interface cable is capable of mating with the DC input 1062 connector (see 3.4.8.2) on the charger. Verify that the DC cable has unterminated leads of length 3 +/- 1 1063 inches on the opposing end. Verify that the DC power interface cable has stranded copper based wire and 1064 is measured to be 6 feet +/- 3 inches long. (See 3.10.3.2) 1065
4.10.3.3 DC extension cord cable (18 ft.). 1067
N/A. 1068
4.10.4 Additional DC inputs. 1070
N/A. 1071
4.10.4.1 NATO slave input power adapter. 1073
Verify through examination that the NATO slave plug meets the requirements of a Type I receptacle per 1074
NATO STANAG 4074 and that no special tools are required. 1075
4.10.4.2 Alligator clips input power adapter. 1077
N/A. 1078
4.10.5 Hard cover. 1080
Through examination verify that the charger has an integrated or removable protective covering for 1081 transportation. 1082
Verify through visual inspection, and/or test, and/or analysis that the system cover: 1084
a. Is the same color as the charger (see 3.4.3). 1085
b. Has all lusterless quick release latching mechanisms and connectors (e.g. snaps, rivets, etc). Hook 1086 and loop straps (e.g. Velcro™) are not to be used. 1087
c. Does not have any sharp protrusions. 1088
d. Is capable of storing the AC input cable and a full set of adapters required for charging batteries. 1089
e. Has a strong carrying handle capable of supporting the weight the charger and AC cord. Apply a 1090 total of 60 lbs below the handle and lift 10 times 1 meter and verify that there is no degradation to 1091 the handle or cover attachment to the charger. 1092
4.10.6 Soft cover. 1094
N/A. 1095
4.10.7 Transportation case. 1097
N/A. 1098
4.11 Repairability. 1100
As stated. 1101
5 PACKAGING 1103
5.1 Packaging. 1105
As stated. 1106
6 NOTES 1108
6.1 Intended use. 1110
The bulk charger is a man-portable universal battery charger with interfaces to support a variety of current 1111 and future military batteries. The bulk charger should be rugged, one man lift when carried, stacked for 1112 storage, or transported in a vehicle. 1113
6.2 Acquisition requirements. 1115
As stated. 1116
6.3 Battery interfaces. 1118
As stated. 1119
6.4 Government-run test. 1121
As stated. 1122
6.5 Random tests. 1124
As stated. 1125
6.6 Lessons learned and other information. 1127
As stated. 1128
6.7 Definitions. 1130
As stated. 1131
6.8 Subject term (key word) listing. 1133
As stated. 1134
7 APPENDIX(ES). 1135
7.1 APPENDIX A 1137
As stated. 1138
File details come from the government source that posted it. Updated .