The EV2812-1100 is a high-output propulsion solution for payload-focused UAVs, advanced multirotors, flight-test aircraft, and OEM development programs requiring expanded thrust capability.
Unit of Measure

Specifications

Stator Size

N/A 2812

KV

N/A 1100 KV

Dimensions

N/A 33.4 x 40 mm (1.31 x 1.57 in)

Configuration

N/A 12N14P

Shaft Diameter

N/A 5 mm

Weight

N/A 78.9 g

Cable Length

N/A 250 mm

Cells

N/A 4S-6S

Series

N/A EV2800

Speed (up to)

N/A 29,100 rpm

Idle Current (20V)

N/A 1.4 A

Maximum Power

N/A 1,375 Watts

Peak Current

N/A 55 A

Resistance

N/A 53.4 mOhm

Lead Wires (AWG)

N/A 18 AWG / 1 mm²

Propeller Performance Data

N/A

Tested Propeller Cell Configuration Max Thrust Electrical Power Current Speed Efficiency Datasheet
6 × 2.5 × 3 4S 618 g 147.0 W 9.12 A 17,400 RPM 4.20 g/W EV2812-1100 – 6×2.5×3 – 4S
6 × 3 × 3 4S 690 g 165.4 W 10.29 A 17,229 RPM 4.17 g/W EV2812-1100 – 6×3×3 – 4S
6 × 3.5 × 3 4S 891 g 225.4 W 14.23 A 16,371 RPM 3.95 g/W EV2812-1100 – 6×3.5×3 – 4S
7 × 4 × 3 4S 1,160 g 277.5 W 17.86 A 15,686 RPM 4.18 g/W EV2812-1100 – 7×4×3 – 4S
7.1 × 4 × 3 4S 1,305 g 310.4 W 20.14 A 15,171 RPM 4.20 g/W EV2812-1100 – 7.1×4×3 – 4S
7.5 × 4 × 2 4S 1,168 g 314.7 W 19.75 A 15,257 RPM 3.83 g/W EV2812-1100 – 7.5×4×2 – 4S
8 × 4 × 3 4S 1,600 g 410.5 W 27.17 A 13,886 RPM 3.90 g/W EV2812-1100 – 8×4×3 – 4S
9 × 4 × 3 4S 1,782 g 456.0 W 30.56 A 13,114 RPM 3.91 g/W EV2812-1100 – 9×4×3 – 4S
10 × 4.5 × 2 4S 2,100 g 543.9 W 37.20 A 11,829 RPM 3.86 g/W EV2812-1100 – 10×4.5×2 – 4S
6 × 2.5 × 3 6S 1,444 g 454.1 W 18.85 A 25,029 RPM 3.18 g/W EV2812-1100 – 6×2.5×3 – 6S
6 × 3 × 3 6S 1,529 g 491.6 W 20.44 A 24,857 RPM 3.11 g/W EV2812-1100 – 6×3×3 – 6S
6 × 3.5 × 3 6S 1,848 g 655.2 W 27.53 A 23,229 RPM 2.82 g/W EV2812-1100 – 6×3.5×3 – 6S
7 × 4 × 3 6S 2,373 g 863.4 W 37.04 A 21,600 RPM 2.75 g/W EV2812-1100 – 7×4×3 – 6S
7.1 × 4 × 3 6S 2,486 g 904.2 W 39.06 A 21,086 RPM 2.75 g/W EV2812-1100 – 7.1×4×3 – 6S
7.5 × 4 × 2 6S 2,257 g 897.1 W 38.52 A 21,171 RPM 2.52 g/W EV2812-1100 – 7.5×4×2 – 6S

* For detailed specifications and motor performance curves, please refer to the complete product specification sheet.

Propeller Reference Guide

N/A

EV2800 Tested Propeller Reference Table
Propeller Reference Diameter (in) Pitch (in) Number of Blades Used With Models
6 × 2.5 × 3 6 in 2.5 in 3 blades EV2810-1100, EV2812-1100
6 × 3 × 3 6 in 3 in 3 blades EV2810-1100, EV2812-1100
6 × 3.5 × 3 6 in 3.5 in 3 blades EV2810-1100, EV2812-1100
7 × 4 × 3 7 in 4 in 3 blades EV2810-1100, EV2812-1100
7.1 × 4 × 3 7.1 in 4 in 3 blades EV2810-1100, EV2812-1100
7.5 × 4 × 2 7.5 in 4 in 2 blades EV2810-1100, EV2812-1100
8 × 4 × 3 8 in 4 in 3 blades EV2810-1100, EV2812-1100
9 × 4 × 3 9 in 4 in 3 blades EV2810-1100, EV2812-1100
10 × 4.5 × 2 10 in 4.5 in 2 blades EV2812-1100

NOTE: Propeller format is shown as diameter × pitch × blade count. For example, 10 × 4.5 × 2 indicates a 10-inch diameter, 4.5-inch pitch, two-blade propeller.

Detailed Propeller Performance Reference

N/A

EV2812-1100
Tested Propeller Cell Configuration Max Thrust Electrical Power Current Speed Efficiency
6 × 2.5 × 3 4S 618 g 147.0 W 9.12 A 17,400 RPM 4.20 g/W
6 × 3 × 3 4S 690 g 165.4 W 10.29 A 17,229 RPM 4.17 g/W
6 × 3.5 × 3 4S 891 g 225.4 W 14.23 A 16,371 RPM 3.95 g/W
7 × 4 × 3 4S 1,160 g 277.5 W 17.86 A 15,686 RPM 4.18 g/W
7.1 × 4 × 3 4S 1,305 g 310.4 W 20.14 A 15,171 RPM 4.20 g/W
7.5 × 4 × 2 4S 1,168 g 314.7 W 19.75 A 15,257 RPM 3.83 g/W
8 × 4 × 3 4S 1,600 g 410.5 W 27.17 A 13,886 RPM 3.90 g/W
9 × 4 × 3 4S 1,782 g 456.0 W 30.56 A 13,114 RPM 3.91 g/W
10 × 4.5 × 2 4S 2,100 g 543.9 W 37.20 A 11,829 RPM 3.86 g/W
6 × 2.5 × 3 6S 1,444 g 454.1 W 18.85 A 25,029 RPM 3.18 g/W
6 × 3 × 3 6S 1,529 g 491.6 W 20.44 A 24,857 RPM 3.11 g/W
6 × 3.5 × 3 6S 1,848 g 655.2 W 27.53 A 23,229 RPM 2.82 g/W
7 × 4 × 3 6S 2,373 g 863.4 W 37.04 A 21,600 RPM 2.75 g/W
7.1 × 4 × 3 6S 2,486 g 904.2 W 39.06 A 21,086 RPM 2.75 g/W
7.5 × 4 × 2 6S 2,257 g 897.1 W 38.52 A 21,171 RPM 2.52 g/W

NOTE: Performance data depends on battery voltage, ESC settings, airflow, mounting conditions, propeller selection, and aircraft design. Use these tables for engineering screening; validate final selections with application-specific testing.

Best-Fit Application

N/A

Model Number Best-Fit Application
EV2810-1100 Compact Multirotor / Inspection UAV
EV2812-1100 Higher-Output UAV

Features & Specifications

N/A Features & Specifications

  • 1100 KV, 2810 and 2812-class motor platforms
  • Compact 33.4 mm frame diameter architecture
  • 12N14P configuration
  • 5 mm shaft diameter
  • 4S–6S battery compatibility
  • Up to 1,375 W maximum power capability
  • Published thrust, power, current, RPM, and efficiency data
  • OEM customization and application support available
  • Defense-compliant sourcing and program support

Applications

N/A Features & Specifications

  • Payload-focused UAV designs
  • Advanced multirotors
  • Inspection and industrial UAV systems
  • Flight-test aircraft
  • OEM development programs