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Skyward 450

By GUIZHOU SUPER ENERGY ERA TECHNOLOGY CO.,LTD ↗

Guizhou Super Energy Era Technology Co., Ltd.’s Skyward 450 is an endurance-focused hybrid solid-liquid electrolyte battery cell measuring 9 × 87 × 187 mm. Rated capacity is 50 Ah and energy density is 450±10 Wh/kg, both at 0.1C and room temperature. Continuous discharge is limited to 0.5C, and it is not a drop-in replacement for standard production airframes.

Manufacturer and modelGuizhou Super Energy Era Technology Co., Ltd. Skyward 450
Product architectureHybrid solid-liquid electrolyte battery cell
ChemistryAnode-free lithium metal (AFLMB)
Dimensions, thickness × width × height9 × 87 × 187 mm
Rated capacity50 Ah0.1C, RT
Nominal voltage3.81 V

Product overview

Guizhou Super Energy Era Technology Co., Ltd.’s Skyward 450 is a hybrid solid-liquid electrolyte battery cell intended for endurance-focused applications, including UAV power systems. It uses anode-free lithium metal (AFLMB) chemistry and measures 9 × 87 × 187 mm in thickness, width and height. Its electrical specifications pair a nominal voltage of 3.81 V with a rated capacity of 50 Ah at 0.1C and room temperature. Energy density is specified as 450±10 Wh/kg under the same conditions.

For procurement and integration, the cell’s discharge limits and cycle life are material constraints. Maximum continuous discharge is 0.5C; the 1C pulse discharge rating applies for 10 seconds at 50℃. Cycle life is 50 cycles at 25℃ under the stated 0.2C/0.5C conditions. The design prioritizes energy density and single-flight endurance, accepting lower discharge rate and cycle life. Planned sortie count therefore matters to lifetime cost, and the Skyward 450 is not a drop-in replacement for standard production airframes.

Specifications

SpecificationValue & conditions
Manufacturer and modelGuizhou Super Energy Era Technology Co., Ltd. Skyward 450
Product architectureHybrid solid-liquid electrolyte battery cell
ChemistryAnode-free lithium metal (AFLMB)
Dimensions, thickness × width × height9 × 87 × 187 mm
Rated capacity50 Ah0.1C, RT
Nominal voltage3.81 V
Energy density450±10 Wh/kg0.1C, RT
Maximum continuous discharge rate0.5C
Pulse discharge rate1C10-second pulse at 50℃
Cycle life50 cycles25℃; 0.2C/0.5C
Airframe integration limitationNot a drop-in replacement for standard production airframes
Application priorityPrioritizes single-flight endurance, with lower discharge rate and cycle life as trade-offs

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