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6S 30000mAh UAV Battery
  • 6S 30000mAh UAV Battery6S 30000mAh UAV Battery
  • 6S 30000mAh UAV Battery6S 30000mAh UAV Battery
  • 6S 30000mAh UAV Battery6S 30000mAh UAV Battery
  • 6S 30000mAh UAV Battery6S 30000mAh UAV Battery
  • 6S 30000mAh UAV Battery6S 30000mAh UAV Battery
  • 6S 30000mAh UAV Battery6S 30000mAh UAV Battery
  • 6S 30000mAh UAV Battery6S 30000mAh UAV Battery
  • 6S 30000mAh UAV Battery6S 30000mAh UAV Battery
  • 6S 30000mAh UAV Battery6S 30000mAh UAV Battery
  • 6S 30000mAh UAV Battery6S 30000mAh UAV Battery

6S 30000mAh UAV Battery

The China 6S 30000mAh UAV Battery is the higher-current 6S step in the HSS capacity matrix, combining 666Wh nominal energy, approximately 2050g finished mass and 90A continuous discharge in a 68 x 78 x 195mm envelope. It is intended for OEM projects where sustained current and installed energy must rise together without moving directly to the larger 40Ah high-energy platform.
666Wh:Nominal Energy
Approx. 2050g:Pack Weight
90A
Continuous Discharge
68mm
Pack Width
Rating: 5.0
(Rating Count: 1)

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.

6S 30000mAh UAV Battery

HSS Energy HSS 6S30Ah front and side product views.

Product Specifications - Electrical and Energy

Parameter

Specification

Product model

HSS 6S30Ah

Battery type / cell

Semi-solid-state lithium battery; CGB10675175-30000mAh

Configuration

6S1P reference configuration

Nominal voltage

22.2V

Nominal capacity

30000mAh / 30Ah

Nominal energy

666Wh

Cell energy density

350Wh/kg individual-cell value

Calculated pack reference

About 325Wh/kg from 666Wh / approx. 2.05kg

Maximum charge current

15A at 0.5C

Charge cutoff voltage

25.5V

Discharge cutoff voltage

15.0V

Continuous discharge

90A at 3C

Maximum discharge

300A at 10C; applicable duration follows the approved configuration


Product Specifications - Operating, Mechanical and Interface

Parameter

Specification

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

Working temperature

-20°C to 55°C

Storage conditions

-20°C to 40°C; below 85% RH

Dimensions (W x T x H)

68 x 78 x 195mm; reference tolerance +/-5mm

Weight

approximately 2050g

Power lead

10AWG, 150mm, optional

Power connector

XT90, optional

Balance harness

22AWG, 150mm, optional

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.

Current Boundary: Sustained Load First, Maximum Current Second

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.

90A continuous

Primary sustained-current screening figure for HSS 6S30Ah.

300A maximum

Short high-demand boundary; duration is configuration- and condition-dependent.

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.

Why 30Ah Exists in the HSS 6S Product Matrix

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.

Selection point

6S16Ah

6S22Ah

6S30Ah

6S40Ah High Energy

Nominal energy

355.2Wh

488.4Wh

666Wh

888Wh

Approx. pack mass

1.48kg

1.62kg

2.05kg

2.35kg

Continuous current

48A

66A

90A

80A

Cell energy density

270Wh/kg

350Wh/kg

350Wh/kg

400Wh/kg

Calculated pack ref.

~240Wh/kg

~301Wh/kg

~325Wh/kg

~378Wh/kg

Pack envelope

50 x 78 x 195

55 x 78 x 195

68 x 78 x 195

70 x 90 x 205

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.

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.

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.

Application Fit: Working 6S Aircraft That Need More Sustained Current

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.

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.

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.

Mechanical and Power-Path Fit

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.

OEM Selection Inputs

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.

When 30Ah Is Not the Right Matrix Slot

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.

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.

Production Process Visibility for OEM customers

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.

6S 30000mAh UAV Battery

Cell-process mixing equipment in the production area.

6S 30000mAh UAV Battery

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.

1

Load Profile

2

Power-Path Review

3

Sample Validation

4

Order Drawing

OEM Configuration Freeze Checklist

Electrical limits

Nominal voltage, cutoff values, continuous current and maximum-current duration.

Mechanical envelope

Finished size, restraint, connector access, cable exit and removal path.

Interface details

Power connector, balance connection, polarity, cable gauge and cable length.

Acceptance plan

Sample criteria, label, charger requirement and released order drawing.

Frequently Asked Questions

What is the main role of HSS 6S30Ah in the product matrix?

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.

Does 350Wh/kg describe the finished battery pack?

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.

Is 300A the continuous discharge rating?

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.

Why would I select 30Ah instead of 40Ah?

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.

What charge settings are specified?

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.

Can XT90, cable length and cable direction be customized?

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.

Is this a drop-in replacement for a proprietary smart UAV battery?

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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