Product
Powertrain modelSITLValidation Report
Database
MotorsPropellersBatteries
DocsBlogAboutPricing
Theme

Physics-accurate electric-UAV powertrain simulation.

  • SDK on GitHub
  • LinkedIn
Theme

Product

  • SITL & mission testing
  • Validation & methodology
  • Plans & pricing
  • Product changelog

Database

  • Motor database
  • Propeller database
  • Battery database

Developers

  • API documentation
  • API reference
  • Python SDK
  • MCP server for AI assistants
  • User guide

Company

  • About ThrustLab
  • Engineering portfolio
  • Engineering articles
  • Contact us

Legal

  • Terms of service
  • Privacy policy
  • Refund policy
© 2026 Upwash LLC·Patent US 2026/0062150 A1·Engineering aid, not for safety-critical or certification use.

We use cookies and analytics tools to understand how you use ThrustLab and improve the experience. Privacy Policy

Motors›KDE KDE1806XF-2350

KDE KDE1806XF-2350

The KDE KDE1806XF-2350 is a 2,350 kv motor with a 18 × 6 mm stator, weighing 18 g and rated to 18 A.

Simulate this motor

Specifications

Identity

BrandKDE
ModelKDE1806XF-2350
kv2,350

Electrical

Max A18
Phase resistance117 mΩ
Poles14
Maker cells—
Curve pack—

Mechanical

Weight0.04 lb
Stator18×6
Stator length6 mm

Limits

Max power—
MotorKDE1806XF-2350This page
Propeller—
Battery—
Throttle%
Charge%
Rotors
Free · no account needed

Performance

No published curves for this part yet

Related

Same maker

  • KDE10218XF-105
  • KDE13218XF-105
  • KDE2304XF-2350
  • KDE2306XF-2050
  • KDE2306XF-2550
  • KDE2315XF-2050

Paired with

—

Same class

  • iFlight XING 1303 5000kV
  • MAD AceRacer FS1404.5 GF-D63-3 4500kV
  • Tempest 1704-1480Kv
  • Tempest 1704-2050Kv
  • Tempest 1704-2600Kv
  • Tempest 1706-1310Kv
See all
Fast modelComputed 2026-10-03prom-rs/0.6.2Validation

The curves here are the Fast model, which every account and every visitor runs without limit. An account also runs the Full model, which solves a database propeller from its measured blade geometry.

Engineering aid — ThrustLab results are physics-based estimates, not certified data. Always bench-test and independently validate before committing a real build to flight. Not for safety-critical or certification use.