N-TET

FC-PBF UAV Propeller

Product Overview
Dimension range
16.1~48.1 in
Max thrust
43.52kgf / peak efficiency: 13.97gf/W
Application
For VTOL platforms that need a smaller propeller footprint while maintaining payload capacity, control response, and wind resistance.
Dimension range: 16.1~48.1 in; maximum thrust: 43.52kgf (3373RPM); peak propeller efficiency: 13.97gf/W (1385RPM).

Suitable for VTOL.

With the same thrust, the blade occupies less space.

Lower flight drag, heavy-load capability, stronger controllability, and better wind resistance.

Technical Specifications

Dimensions

16.1~48.1 in

Test example

Example 42x16.5 (28.33℃, 1009.6hPa, 37.72%Rh)

Performance table

ParameterDescription
Speed (RPM)1385
Thrust (kgf)6.92
Shaft power (W)495.17
Propeller efficiency (gf/W)13.97
ParameterDescription
Speed (RPM)1850
Thrust (kgf)12.48
Shaft power (W)1194.78
Propeller efficiency (gf/W)10.44
ParameterDescription
Speed (RPM)2314
Thrust (kgf)19.77
Shaft power (W)2374.82
Propeller efficiency (gf/W)8.32
ParameterDescription
Speed (RPM)2778
Thrust (kgf)28.73
Shaft power (W)4139.22
Propeller efficiency (gf/W)6.94
ParameterDescription
Speed (RPM)3229
Thrust (kgf)39.43
Shaft power (W)6687.60
Propeller efficiency (gf/W)5.90
ParameterDescription
Speed (RPM)3373
Thrust (kgf)43.52
Shaft power (W)7710.32
Propeller efficiency (gf/W)5.64

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.

Home/Drone Accessories/FC-PBF UAV Propeller
FC-PBF UAV Propeller
Dimension range: 16.1~48.1 in
Max thrust: 43.52kgf / peak efficiency: 13.97gf/W
Applications: For VTOL platforms that need a smaller propeller footprint while maintaining payload capacity, control response, and wind resistance.
Get quotation
Dimension range: 16.1~48.1 in; maximum thrust: 43.52kgf (3373RPM); peak propeller efficiency: 13.97gf/W (1385RPM).

Overview

Suitable for VTOL.

With the same thrust, the blade occupies less space.

Lower flight drag, heavy-load capability, stronger controllability, and better wind resistance.

Technical Specifications

Dimensions
16.1~48.1 in
Test example
Example 42x16.5 (28.33℃, 1009.6hPa, 37.72%Rh)
Performance table
Speed (RPM)1385
Thrust (kgf)6.92
Shaft power (W)495.17
Propeller efficiency (gf/W)13.97
Speed (RPM)1850
Thrust (kgf)12.48
Shaft power (W)1194.78
Propeller efficiency (gf/W)10.44
Speed (RPM)2314
Thrust (kgf)19.77
Shaft power (W)2374.82
Propeller efficiency (gf/W)8.32
Speed (RPM)2778
Thrust (kgf)28.73
Shaft power (W)4139.22
Propeller efficiency (gf/W)6.94
Speed (RPM)3229
Thrust (kgf)39.43
Shaft power (W)6687.60
Propeller efficiency (gf/W)5.90
Speed (RPM)3373
Thrust (kgf)43.52
Shaft power (W)7710.32
Propeller efficiency (gf/W)5.64

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.

📝 Get Solution & Quotation💬 WhatsApp