130+ engineering specialists
Dedicated propulsion engineers supporting projects from prototype validation to production deployment
Heavy-Lift UAV Propulsion Solutions
Complete propulsion systems covering 25–125 kg thrust classes for multirotor, VTOL, and manned eVTOL platforms.
Reliable Design Built for Heavy Lift
Heavy-Lift Mission Challenges
Sustained heavy-load operation leads to heat buildup and thrust derating.
Complex operating conditions continuously reduce available thrust margin.
Propulsion system validation increases integration complexity and development timelines.
T-MOTOR Solutions
Magneto-thermal coupled simulation and optimized cooling architecture help reduce temperature rise and maintain stable thrust output during continuous heavy-load operation.
Redundancy-oriented propulsion design helps reserve additional thrust headroom for complex operating conditions and improved flight safety.
Factory pre-matched propulsion systems and validated recommended configurations help reduce integration complexity and shorten deployment cycles.
Heavy-Lift Propulsion Solutions
No standard products match your current filter selection
Contact Our EngineersCustom Heavy-Lift Propulsion Systems
T-MOTOR provides customized heavy-lift propulsion system support for different payload, endurance, and mission requirements.
Customization Scope
Motor parameters:
operating voltage, KV rating, form factor
ESC protocol adaptation:
CAN, PWM, or custom protocols
Propeller customization:
pitch, diameter, material
Full-system integration:
complete propulsion packages designed for your airframe
Engineering Support
Rapid configuration validation
Propulsion platform data enables fast validation of voltage, propeller, and ESC combinations
Flexible project support
No minimum order quantity requirements for different development stages and project scales
Contact Our Propulsion Engineers
Submit your project requirements and T-MOTOR’s engineering team will provide propulsion configuration recommendations based on payload, endurance, platform architecture, and mission requirements.