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HAKRC 4279 14S 80A Airplane ESC

By Shenzhen Haike Technology Co., Ltd. ↗

The HAKRC 4279 14S 80A Airplane ESC is a fixed-wing monobloc speed controller with 6S–14S LiPo input and an integrated 5V BEC. Measuring 59 × 43mm and weighing 63g, it supports several PWM and digital control protocols. Its 80A continuous-current specification carries a 41-second closed-incubator test qualification.

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HAKRC 4279 14S 80A Airplane ESC circuit board
HAKRC 4279 14S 80A Airplane ESC circuit board
Product identity and purposeHAKRC 4279 14S 80A Airplane ESC, a monobloc electronic speed controller for fixed-wing aircraft.
Size59 * 43mm
Net weight of product63g
ESC firmwareHAKRC-AT4G-Rev.32.9-MUlti
Protocol supportPWM, Oneshot125, Oneshot42, Multishot, Dshot150, Dshot300, Dshot600
Input voltage6S-14S LipoLiPo battery input.

Product overview

The HAKRC 4279 14S 80A Airplane ESC is a monobloc electronic speed controller for fixed-wing aircraft. Its specified size is 59 × 43mm and its net weight is 63g, defining the component’s space and mass requirements for installation. It accepts 6S–14S LiPo input and incorporates a BEC specified at 5V, 8A, with a 15A maximum. Control interfaces include PWM, Oneshot125, Oneshot42, Multishot and Dshot150/300/600, with HAKRC-AT4G-Rev.32.9-MUlti firmware specified for the controller.

The electronics combine an AT32F421K8U7 processor running at up to 120MHz with three SLM21867 drivers and parallel 80V MOS devices. A six-layer PCB with 2oz copper, resin-plugged construction, metallized edging and added copper strips forms the current-carrying architecture. Japanese Murata capacitors provide filtering, while an industrial-grade DC-DC converter is described as resistant to high temperatures. The continuous-current specification is 80A under a closed-incubator test lasting 41 seconds; peak current is 100A. That stated test duration is a material qualification when sizing the aircraft’s propulsion installation.

Specifications

SpecificationValue & conditions
Product identity and purposeHAKRC 4279 14S 80A Airplane ESC, a monobloc electronic speed controller for fixed-wing aircraft.
Size59 * 43mm
Net weight of product63g
ESC firmwareHAKRC-AT4G-Rev.32.9-MUlti
Protocol supportPWM, Oneshot125, Oneshot42, Multishot, Dshot150, Dshot300, Dshot600
Input voltage6S-14S LipoLiPo battery input.
BEC5V 8A MAX:15A
Continuous current80A (closed incubator test, 41s last)Closed incubator test, lasting 41s.
Peak current100A
Main control processorAT32F421K8U7, running at up to 120MHz.
Driver configurationThree SLM21867 drivers.
PCB constructionSix-layer PCB with 2oz copper.
PCB fabricationResin-plugged PCB construction with metallized edging.
MOS configurationParallel 80V MOS devices with high-current capability and low internal resistance.
DC-DC converterIndustrial-grade DC-DC converter with high-temperature resistance.
CapacitorsJapanese Murata capacitors for filtering.
Copper stripsEquipped with copper strips to increase current-carrying capacity.
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