Load and charging
ER087187H040A lists 3C continuous discharge, 7C pulse discharge for 10 seconds, and a 1C continuous charge rate. Compare those separate ratings with your load and charging profile.

SEMI-SOLID-STATE / POUCH CELL
40Ah semi-solid-state pouch cell
ER087187H040A is a 40Ah semi-solid-state pouch cell with a 3.46V voltage platform, 3C continuous discharge rating and 380Wh/kg listed specific energy. Its dimensions are 10.1 × 87 × 187mm, with a listed weight of 367g.
01 / TECHNICAL OVERVIEW
Model-specific values for ER087187H040A. Review the voltage range, load rating, mechanical envelope and cycle duty together.
Listed cell weight: 367g. Confirm tab geometry, dimensional tolerances and swelling allowance for the assembly.
| Model | ER087187H040A |
|---|---|
| Cell format / technology | Pouch / semi-solid-state |
| Nominal capacity | 40 Ah |
| Voltage platform | 3.46 V |
| Voltage range | 2.5–4.25 V |
| Continuous discharge rate | 3C |
| Pulse discharge rate | 7C for 10 seconds |
| Continuous charge rate | 1C |
| Cycle life | ≥ 500 cycles at 80% SOH |
| Listed specific energy | 380 Wh/kg |
| Dimensions (T × W × H) | 10.1 × 87 × 187 mm |
| Listed weight | 367 g |
| Discharge temperature | -40 to 60 °C |
Pulse discharge: 7C for 10 seconds. Assess pulse recovery, thermal management, SOC and cut-off conditions for the selected duty.
Cycle life is listed at 80% SOH. Discharge temperature applies to discharge; match charging conditions to the project specification. Voltage range is not a complete charging procedure.
Specific energy is the listed product-data value. Do not use capacity × voltage platform to replace it or infer a guaranteed energy value.
02 / ENGINEERING SELECTION
ER087187H040A lists 3C continuous discharge, 7C pulse discharge for 10 seconds, and a 1C continuous charge rate. Compare those separate ratings with your load and charging profile.
The 10.1 × 87 × 187mm envelope and 367g listed weight are selection inputs. Review the ≥500-cycle value at 80% SOH against the intended cycle duty and complete battery-system design.
Use the aircraft voltage, load profile, mass budget, installation space and environment to evaluate this cell. A specific aircraft or device requires its own system-level validation.
UAV application considerations03 / TECHNICAL DOCUMENTATION
Include ER087187H040A, the intended application, destination market and the documents or test evidence needed by your engineering team.
SICA ENERGY / START A PROJECT
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