6S 30000mAh UAV Battery supplied by HSS Energy is a 22.2V, 30Ah semi-solid-state pack built around a 350Wh/kg individual-cell platform. Nominal energy is 666Wh and finished-pack mass is approximately 2.05kg, giving a calculated complete-pack reference of about 325Wh/kg. The 68mm width keeps the package materially narrower than the 40Ah high-energy platform while the verified 90A continuous rating gives this SKU a different role from the lighter 16Ah and 22Ah options.
The primary buying reason is not maximum capacity alone. HSS 6S30Ah is positioned for custom 6S aircraft programs that need a stronger sustained-current step while remaining inside a familiar 22.2V architecture. Final suitability still depends on aircraft voltage limits, steady and maximum current, maximum-current duration, battery-bay geometry, connector, charger profile, temperature and sample validation.
HSS Energy HSS 6S30Ah front and side product views.
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Parameter |
Specification |
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Product model |
HSS 6S30Ah |
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Battery type / cell |
Semi-solid-state lithium battery; CGB10675175-30000mAh |
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Configuration |
6S1P reference configuration |
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Nominal voltage |
22.2V |
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Nominal capacity |
30000mAh / 30Ah |
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Nominal energy |
666Wh |
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Cell energy density |
350Wh/kg individual-cell value |
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Calculated pack reference |
About 325Wh/kg from 666Wh / approx. 2.05kg |
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Maximum charge current |
15A at 0.5C |
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Charge cutoff voltage |
25.5V |
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Discharge cutoff voltage |
15.0V |
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Continuous discharge |
90A at 3C |
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Maximum discharge |
300A at 10C; applicable duration follows the approved configuration |
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Parameter |
Specification |
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Cycle life reference |
Approx. 200-400 cycles; capacity typically declines to about 80% of initial rated capacity by the end of this range under specified conditions |
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Working temperature |
-20°C to 55°C |
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Storage conditions |
-20°C to 40°C; below 85% RH |
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Dimensions (W x T x H) |
68 x 78 x 195mm; reference tolerance +/-5mm |
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Weight |
approximately 2050g |
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Power lead |
10AWG, 150mm, optional |
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Power connector |
XT90, optional |
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Balance harness |
22AWG, 150mm, optional |
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Balance connector |
XH-7P for B0-B6, optional |
Cycle-life results vary with charge/discharge rate, depth of discharge, temperature, storage practice and end-of-life criteria. Use the test and acceptance conditions applicable to the approved ordered configuration.
For this semi solid state UAV battery, the verified continuous rating is 90A at 3C. The 300A value is the 10C maximum-discharge rating and should not be treated as continuous current. Applicable maximum-current duration is defined according to the approved battery configuration, starting condition, cooling, temperature and aircraft duty cycle. Provide measured current logs whenever the propulsion system approaches the upper current boundary.
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90A continuous Primary sustained-current screening figure for HSS 6S30Ah. |
300A maximum Short high-demand boundary; duration is configuration- and condition-dependent. |
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15A charge limit 0.5C maximum charge current with 25.5V cutoff. |
68 x 78 x 195mm Mechanical envelope to freeze on the aircraft installation drawing. |
HSS 6S30Ah is not a scaled-up 22Ah page and it is not a reduced 40Ah page. Its matrix role is higher sustained current inside the 6S family. The comparison below is product-family selection guidance based on verified energy, mass, continuous current, cell platform and mechanical envelope; it is not an automatic aircraft-compatibility statement.
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Selection point |
6S16Ah |
6S22Ah |
6S30Ah |
6S40Ah High Energy |
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Nominal energy |
355.2Wh |
488.4Wh |
666Wh |
888Wh |
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Approx. pack mass |
1.48kg |
1.62kg |
2.05kg |
2.35kg |
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Continuous current |
48A |
66A |
90A |
80A |
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Cell energy density |
270Wh/kg |
350Wh/kg |
350Wh/kg |
400Wh/kg |
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Calculated pack ref. |
~240Wh/kg |
~301Wh/kg |
~325Wh/kg |
~378Wh/kg |
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Pack envelope |
50 x 78 x 195 |
55 x 78 x 195 |
68 x 78 x 195 |
70 x 90 x 205 |
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Matrix role |
Compact 6S |
Mid-capacity |
Higher-current 6S |
High installed energy |
Compared with HSS 6S22Ah, the 30Ah platform adds 177.6Wh nominal energy and 24A continuous current while increasing approximate pack mass by about 430g and width by 13mm. Compared with the 40Ah High Energy platform, HSS 6S30Ah carries 222Wh less nominal energy but has a 10A higher continuous-current rating, is about 300g lighter, and uses a thinner and shorter 68 x 78 x 195mm envelope. This is why the 6S high current UAV battery role belongs to the 30Ah slot rather than being duplicated across the family.
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Choose 16Ah When minimum HSS 6S mass and the narrowest 50mm width are the first screening priorities. |
Choose 22Ah When a mid-capacity step is needed before moving to the wider 30Ah class. |
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Choose 30Ah When 666Wh and 90A continuous current justify the added width and mass. |
Choose 40Ah High Energy When total installed energy and complete-pack specific-energy positioning matter more than the highest continuous-current figure in this 6S set. |
The 30Ah drone battery position is aimed at custom 6S aircraft where sustained electrical demand is a central selection factor. Primary fit is a custom 6S utility or working multirotor platform that can accommodate approximately 2.05kg battery mass and the 68 x 78 x 195mm package. Secondary evaluation can include compatible agricultural, industrial observation or large-format multirotor projects when the complete voltage, current, mechanical and charger requirements are confirmed.
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Primary role Utility / working 6S multirotor with a verified need for 90A continuous current. |
Secondary role 1 Custom agricultural or spraying platform already engineered around a compatible 6S voltage architecture. |
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Secondary role 2 Large-format multirotor project where 666Wh installed energy and the 68mm width fit the aircraft package. |
Do not assume A proprietary smart-battery aircraft may require communication, locking, monitoring or charger functions beyond voltage and capacity. |
A UAV Lithium battery pack should be evaluated as part of the aircraft installation, not as an isolated capacity number. Confirm center of gravity, restraint, connector access, cable bend radius, cooling, battery removal path and maximum installed envelope. The reference 10AWG power lead and XT90 connector are options, so final cable length, polarity, exit direction and connector arrangement should be frozen on the approved drawing.
For a 22.2V 30000mAh UAV battery review, send HSS Energy the aircraft or project type, operating voltage range, steady current, maximum current and duration, target mission profile, maximum battery mass, battery-bay drawing, connector, cable length, charger information, operating temperature, sample quantity and destination.
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Mass ceiling If approximately 2.05kg is outside the aircraft battery-mass limit, screen the lighter 22Ah platform first. |
Energy-first mission If 888Wh installed energy is the main priority and 80A continuous current is sufficient, evaluate the 40Ah High Energy platform. |
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Voltage mismatch If the propulsion and charger are engineered for 8S, move to the HSS 8S matrix rather than adapting a 6S pack by assumption. |
Proprietary interface If communication, locking or smart-charger functions are mandatory, provide the interface documents before battery selection. |
For this higher-current 6S platform, process visibility helps OEM customers understand how cell-process preparation and electrode-processing equipment fit into the manufacturing workflow. The workshop photographs below show production equipment and organized process areas. They are presented as manufacturing context only; final product quality requirements are defined by the approved specification and sample acceptance plan.
Cell-process mixing equipment in the production area.
Electrode-processing equipment in the production workflow.
From Current Requirement to Released Configuration
The commercial path for HSS 6S30Ah should start with the aircraft current profile rather than with capacity alone. HSS Energy can then freeze the electrical limits, mechanical envelope, cable and connector configuration, label, charger requirement and sample acceptance criteria before the order drawing is released.
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1 Load Profile |
2 Power-Path Review |
3 Sample Validation |
4 Order Drawing |
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Electrical limits Nominal voltage, cutoff values, continuous current and maximum-current duration. |
Mechanical envelope Finished size, restraint, connector access, cable exit and removal path. |
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Interface details Power connector, balance connection, polarity, cable gauge and cable length. |
Acceptance plan Sample criteria, label, charger requirement and released order drawing. |
It is the higher-current 6S option in the current HSS capacity matrix. It combines 666Wh nominal energy with 90A continuous discharge and a 68 x 78 x 195mm envelope, positioned between the lighter 22Ah platform and the higher-installed-energy 40Ah platform.
No. 350Wh/kg is the individual-cell energy-density value. Based on 666Wh nominal energy and approximately 2.05kg finished mass, the calculated complete-pack reference is about 325Wh/kg.
No. Continuous discharge is 90A at 3C. The 300A figure is maximum discharge at 10C, and applicable duration follows the approved configuration and operating conditions.
Select 30Ah when the 90A continuous-current rating, approximately 300g lower mass and smaller 68 x 78 x 195mm envelope are more important than the 40Ah platform's higher installed energy and higher calculated pack specific-energy reference.
Maximum charge current is 15A at 0.5C with a 25.5V charge cutoff. Use the charger profile and balance connection approved for the ordered 6S configuration.
The reference configuration includes an optional XT90 connector, 10AWG 150mm power lead and XH-7P balance connection. Final connector, cable length, polarity and exit direction can be reviewed and recorded on the approved order drawing.
Not automatically. Proprietary systems may require communication, enclosure, locking, monitoring or charging functions beyond voltage and capacity. Send the aircraft battery interface and charger details for review.
Send the aircraft current profile, battery-bay drawing and charger details so HSS Energy can confirm whether HSS 6S30Ah is the correct matrix position for sampling.
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