Description Catalog Reviews

SIYI E8 Integrated Propulsion System for Agricultural UAV Platforms

PriceOn request
ModelE8
Product typeIntegrated UAV propulsion system
Key hardware80A FOC
Input supplyCatalog recommended battery: 12–14S LiPo
Interface or platformCAN; PWM signal input listed
ConfigurationESC firmware upgrade: Supported
Rated specificationCatalog maximum thrust, one axis: 18.5kg
WeightUnit mass excluding propeller: 960g
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AGRICULTURAL UAV PROPULSION

Start with the arm, propeller envelope and complete unit

SIYI E8 is an integrated motor-and-ESC propulsion unit for larger civilian UAV platforms, including agricultural aircraft. Its 110KV motor is paired in the catalog with a 32 × 12-inch folding propeller. The listed arm-tube fit is 40mm, placing the physical installation in a different class from a compact FPV motor or a small camera-drone propulsion set.

When comparing units, put the arm diameter and propeller envelope ahead of the headline thrust number. Those dimensions determine whether the offered hardware is relevant to an existing frame and whether its service parts can be stocked alongside equipment already in use.

SIYI E8 propulsion unit with folded propeller
E8 integrated propulsion illustration extracted from the manufacturer catalog; the pictured propeller arrangement is identified in the offer.

Complete propulsion unit

The catalog mass is 960g excluding the propeller. This is the relevant unit-level figure for the mounted motor and ESC arrangement; it should not be replaced by the motor-only number when preparing an aircraft mass budget.

Motor and propeller

The motor table lists 526g for the motor, while the propeller table gives 240g for the 32 × 12-inch propeller. Keep those separate component figures attached to their labels when comparing replacements or spare assemblies.

Control and connection

CAN communication and PWM signal input are documented. Ask for the control connection and harness required by the proposed flight controller, with the motor-unit revision identified on the offer.

Read the electrical limits with their conditions

The ESC is described as an 80A FOC unit. Its tabulated continuous-current figure is 80A with good heat dissipation, and its 150A peak is limited to three seconds. These are different conditions. A short peak figure should not be used as a continuous thermal rating when comparing an alternative ESC or power arrangement.

The supplied catalog recommends a 12–14S LiPo platform and gives 63V as the ESC maximum working voltage. Confirm the complete voltage envelope of the proposed supply against the offered revision. A cell-count label and a maximum-voltage limit each convey part of that electrical specification.

One-axis figures stay with one propulsion unit

The E8 maximum-thrust figure is 18.5kg per axis. The catalog's recommended takeoff-weight band is also stated per axis, at 5–8kg. Neither statement is an independent payload rating for a finished aircraft. Ask which exact motor, ESC and propeller combination the supplier is quoting before comparing the numbers with another propulsion family.

E8 motor housing and folding hub detail
Detail cropped from the same catalog illustration, showing the motor housing and propeller hub; package quantities remain separate.

Specify service parts at the same time

For an agricultural fleet or a replacement order, provide the frame's arm dimensions, existing E8 identification and the preferred propeller arrangement. List the required unit count and the number of spare propellers, hubs or other service parts separately. Include the flight controller and available control interface so that the supplied lead arrangement can be checked.

Request the environmental specification for the exact assembly and its connectors if exposed agricultural work is part of the requirement. Keep any component protection code attached to the part it describes, and identify the motor-unit revision and the intended maintenance conditions on the offer.

E8 purchasing questions

Does the 960g figure include the propeller?

No. The catalog identifies 960g as unit mass excluding the propeller and lists the propeller separately at 240g.

Can the 150A figure be compared with a continuous ESC rating?

It is a three-second peak figure. The separately listed continuous rating includes a good-heat-dissipation condition.

What helps identify a replacement unit?

Provide the existing motor and ESC markings, arm dimensions, propeller type and connector photographs. That gives a more precise basis than the aircraft brand alone.

SIYI E8 specifications

Catalog maximum thrust, one axis18.5kg
Catalog recommended takeoff weight, one axis5–8kg
Catalog recommended battery12–14S LiPo
Arm-tube diameter40mm
Unit mass excluding propeller960g
ESC model80A FOC
Maximum working voltage63V
ESC continuous current80A with good heat dissipation
ESC peak current150A for 3 seconds
CommunicationCAN; PWM signal input listed
Motor KV110rpm/V
Motor mass526g
Propeller dimensions32 × 12in
Propeller mass240g
Catalog rated input power1042W
Catalog rated output power908W
Power-cable length1000mm
Signal-cable length1100mm
PWM signal voltage3.3V / 5V
PWM pulse range1050–1950μs
PWM frequency50–500Hz
ESC firmware upgradeSupported
Digital throttleCAN throttle
Motor stator81 × 18mm
Motor slot/pole configuration36N40P

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