Product overview
The YATTOX 6S 15000mAh 22.2V LiPo Battery is a power pack for UAV installations. Its six-cell series architecture combines lithium polymer chemistry with a rated capacity of 15,000mAh (15Ah) and nominal stored energy of 333Wh. The configuration carries a 10C discharge marking. Aircraft integration requires motors, ESCs, power distribution and charging equipment suitable for the pack’s full charging and discharge voltage range, because 22.2V describes nominal voltage rather than a constant operating voltage.
Physical installation depends on the supplied pack’s weight, external dimensions, securing method, connector and polarity matching the aircraft’s battery space and weight allowance. Those mechanical details and the final connector configuration require confirmation for the supplied version. Continuous and transient current limits also need to match the aircraft load and complete wiring path. Available energy varies with temperature, discharge limits and aircraft power demand; endurance additionally depends on installed battery mass, propulsion efficiency and mission load.
Specifications
| Specification | Value & conditions |
|---|---|
| Battery chemistry | Lithium Polymer (LiPo) |
| Series configuration | 6S |
| Nominal voltage | 22.2V |
| Rated capacity | 15,000mAh (15Ah) |
| Nominal energy | 333Wh |
| Discharge rating | 10C (label rating)Product-label rating. |
| Electrical integration | Motors, ESCs, power distribution and charger must accommodate the six-cell LiPo voltage range; 22.2V is nominal rather than a fixed operating voltage.Throughout the pack's charging and discharge range. |
| Mechanical and connector configuration | Pack weight, external dimensions, securing method and connector polarity require configuration-specific confirmation for aircraft installation.For the supplied version. |
| Usable energy limitation | Available energy depends on discharge limits, temperature and aircraft power demand.Under the applicable discharge limits, temperature and aircraft power profile. |
| Current delivery integration | Continuous and transient current limits, connectors and cabling must be matched to the expected load.For the expected aircraft load demand. |
