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FC-C2U UAV Propeller

Product Overview
Dimension range
16~47 in
Max thrust
38.70kgf / peak efficiency: 12.63gf/W
Application
For fixed-wing and hybrid-wing UAVs requiring heavy payload capability, high thrust, and large pitch.
Dimension range: 16~47 in; maximum thrust: 38.70kgf (7279RPM); peak propeller efficiency: 12.63gf/W (2309RPM).

Suitable for fixed-wing and hybrid-wing UAVs.

Heavy payload, high thrust, and large pitch.

Technical Specifications

Dimensions

16~47 in

Test example

Example 26x16 (10.24℃, 1019.8hPa, 43.09%Rh)

Performance table

ParameterDescription
Speed (RPM)2309
Thrust (kgf)3.89
Shaft power (W)308.06
Propeller efficiency (gf/W)12.63
ParameterDescription
Speed (RPM)3544
Thrust (kgf)9.23
Shaft power (W)1225.87
Propeller efficiency (gf/W)7.53
ParameterDescription
Speed (RPM)4417
Thrust (kgf)14.28
Shaft power (W)2480.72
Propeller efficiency (gf/W)5.76
ParameterDescription
Speed (RPM)5099
Thrust (kgf)19.24
Shaft power (W)3987.25
Propeller efficiency (gf/W)4.82
ParameterDescription
Speed (RPM)5645
Thrust (kgf)23.86
Shaft power (W)5621.94
Propeller efficiency (gf/W)4.24
ParameterDescription
Speed (RPM)6103
Thrust (kgf)28.09
Shaft power (W)7439.41
Propeller efficiency (gf/W)3.78
ParameterDescription
Speed (RPM)6646
Thrust (kgf)32.36
Shaft power (W)10221.99
Propeller efficiency (gf/W)3.17
ParameterDescription
Speed (RPM)7279
Thrust (kgf)38.70
Shaft power (W)14599.16
Propeller efficiency (gf/W)2.65

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Please fill out the form below, and we can satisfy any of your needs including equipment selection, custom solution design, technical support, or after-sales service. We will contact you as soon as possible.

Home/Drone Accessories/FC-C2U UAV Propeller
FC-C2U UAV Propeller
Dimension range: 16~47 in
Max thrust: 38.70kgf / peak efficiency: 12.63gf/W
Applications: For fixed-wing and hybrid-wing UAVs requiring heavy payload capability, high thrust, and large pitch.
Get quotation
Dimension range: 16~47 in; maximum thrust: 38.70kgf (7279RPM); peak propeller efficiency: 12.63gf/W (2309RPM).

Overview

Suitable for fixed-wing and hybrid-wing UAVs.

Heavy payload, high thrust, and large pitch.

Technical Specifications

Dimensions
16~47 in
Test example
Example 26x16 (10.24℃, 1019.8hPa, 43.09%Rh)
Performance table
Speed (RPM)2309
Thrust (kgf)3.89
Shaft power (W)308.06
Propeller efficiency (gf/W)12.63
Speed (RPM)3544
Thrust (kgf)9.23
Shaft power (W)1225.87
Propeller efficiency (gf/W)7.53
Speed (RPM)4417
Thrust (kgf)14.28
Shaft power (W)2480.72
Propeller efficiency (gf/W)5.76
Speed (RPM)5099
Thrust (kgf)19.24
Shaft power (W)3987.25
Propeller efficiency (gf/W)4.82
Speed (RPM)5645
Thrust (kgf)23.86
Shaft power (W)5621.94
Propeller efficiency (gf/W)4.24
Speed (RPM)6103
Thrust (kgf)28.09
Shaft power (W)7439.41
Propeller efficiency (gf/W)3.78
Speed (RPM)6646
Thrust (kgf)32.36
Shaft power (W)10221.99
Propeller efficiency (gf/W)3.17
Speed (RPM)7279
Thrust (kgf)38.70
Shaft power (W)14599.16
Propeller efficiency (gf/W)2.65

Get Solution & Quotation

Please fill out the form below, and we can satisfy any of your needs including equipment selection, custom solution design, technical support, or after-sales service. We will contact you as soon as possible.

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