400Wh/kg Series Semi-Solid State High Energy Density Battery Pack
| Battery Model | Capacity / Energy | Nominal Voltage | Discharge Cut-off Voltage | Dimension | Weight | Pack Energy Density | Max Continuous Discharge Current(2C) | Max Pulse Current (≤15S) |
| TARBG4008K06S10X | 8Ah / 177.6Wh | 6S 22.2V | 15V | 180 x 65.5 x 26mm | 540g | 328.89Wh/kg | 24A | 40A |
| TARBG4008K08S10X | 8Ah / 236.8Wh | 8S 29.6V | 20V | 182 x 65.5 x 34mm | 710g | 333.52Wh/kg | 24A | 40A |
| TARBG4008K12S10X | 8Ah / 355.2Wh | 12S 44.4V | 30V | 187 x 66 x 52mm | 1070g | 331.96Wh/kg | 24A | 40A |
| TARBG4012K06S10X | 12Ah / 266.4Wh | 6S 22.2V | 15V | 194 x 71.5 x 31mm | 770g | 345.97Wh/kg | 36A | 60A |
| TARBG4012K08S10X | 12Ah / 355.2Wh | 8S 29.6V | 20V | 196 x 71.5 x 41mm | 1020g | 348.24Wh/kg | 36A | 60A |
| TARBG4012K12S10X | 12Ah / 532.8Wh | 12S 44.4V | 30V | 201 x 72 x 61mm | 1540g | 345.97Wh/kg | 36A | 60A |
| TARBG4016K06S10X | 16Ah / 355.2Wh | 6S 22.2V | 15V | 185 x 71.5 x 41mm | 990g | 358.79Wh/kg | 48A | 80A |
| TARBG4016K08S10X | 16Ah / 473.6Wh | 8S 29.6V | 20V | 187 x 71.5 x 54mm | 1300g | 364.31Wh/kg | 48A | 80A |
| TARBG4016K12S10X | 16Ah / 710.4Wh | 12S 44.4V | 30V | 192 x 72 x 80mm | 2050g | 346.54Wh/kg | 48A | 80A |
| TARBG4030K06S10X | 30Ah / 666Wh | 6S 22.2V | 15V | 205 x 91.5 x 49mm | 1880g | 354.26Wh/kg | 60A | 90A |
| TARBG4030K08S10X | 30Ah / 888Wh | 8S 29.6V | 20V | 207 x 91.5 x 65mm | 2500g | 355.20Wh/kg | 60A | 90A |
| TARBG4030K12S10X | 30Ah / 1332Wh | 12S 44.4V | 30V | 212 x 92 x 108mm | 3800g | 350.53Wh/kg | 90A | 150A |
| TARBG4036K06S10X | 36Ah / 799.2Wh | 6S 22.2V | 15V | 205 x 91.5 x 58mm | 2240g | 356.79Wh/kg | 60A | 90A |
| TARBG4036K08S10X | 36Ah / 1065.6Wh | 8S 29.6V | 20V | 207 x 91.5 x 77mm | 2980g | 357.58Wh/kg | 60A | 90A |
| TARBG4036K12S10X | 36Ah / 1598.4Wh | 12S 44.4V | 30V | 212 x 92 x 126mm | 4530g | 352.85Wh/kg | 72A | 150A |
| TARBG4041K06S10X | 41Ah / 910.2Wh | 6S 22.2V | 15V | 193 x 85.5 x 69mm | 2450g | 371.51Wh/kg | 60A | 90A |
| TARBG4041K12S10X | 41Ah / 1820.4Wh | 12S 44.4V | 30V | 198 x 86 x 145mm | 5000g | 364.08Wh/kg | 82A | 150A |
| TARBG4010706S10X | 107Ah / 2375.4Wh | 6S 22.2V | 15V | 285 x 151.1 x 71mm | 6600g | 359.91Wh/kg | 100A | 150A |
| TARBG4010708S10X | 107Ah / 3167.2Wh | 8S 29.6V | 20V | 287 x 151.1 x 100.5mm | 8780g | 360.73Wh/kg | 100A | 150A |
| TARBG4010712S10X | 107Ah / 4750.8Wh | 12S 44.4V | 30V | 292 x 152 x 152mm | 13400g | 354.54Wh/kg | 100A | 150A |
*Pack energy density is calculated from the listed nominal energy and total pack weight. The table uses connector-limited discharge currents for the standard XT90S-F and AS150U-F configurations. Ideal electrical capability can be higher and must be validated with the selected connector, cable, thermal design and aircraft load profile. Maximum pulse-current duration is 15 seconds. The listed 6S configurations support G-Tech; the listed 8S and 12S configurations are standard non-G-Tech packs.
*Nominal capacity is measured at 0.5C. Standard charge temperature: 10 to 50°C. Standard discharge temperature: -20 to 60°C. Storage temperature: -20 to 35°C for less than three months. Published cycle life: more than 300 cycles. Packaging: soft pack.
● Cell technology platform with energy density up to 400Wh/kg
● More than 300 cycles for lower replacement frequency in commercial UAV fleets
● Discharge operation from -20°C to 60°C for demanding field environments
● G-Tech support on selected 6S models for intelligent battery and charger integration
● Customizable capacity, voltage, dimensions, cables, connectors and charging solutions
●Tattu TA3200 Series dual-channel drone battery chargers for 6-14S pouch cell batteries.
Discover more UAV / Drone Chargers: Battery Charger
The 400Wh/kg figure identifies the cell technology platform. Complete pack weight also includes tabs, cables, connectors, insulation, protection and structural components, so pack-level energy density varies by configuration.
The series is suitable for mapping, surveying, inspection, delivery, agricultural, monitoring, multirotor, fixed-wing and VTOL platforms when voltage, current, weight and dimensions are correctly matched.
The public table uses the current supported by the standard connector configuration. Actual system current can be limited by the connector, cable, contact resistance, thermal design and permitted pulse duration, even when the battery cells have higher theoretical capability.
Provide the aircraft takeoff weight, payload, motor and ESC configuration, average and peak current, peak duration, target flight time, battery compartment, connector, operating temperature and current battery specification. Flight logs are especially useful.
