IPET IV9(7224)
An integrated IV9 (7224) propulsion system combining the motor, FOC IV150A ESC, and validated propeller configurations for 28–35 kg fixed-wing and VTOL UAVs. Designed for higher cruise thrust, stable thermal performance, and real-time propulsion feedback.
Engineering Fit Check
Use these parameters for initial cruise-propulsion selection. Final sizing should be verified against airframe drag, cruise speed, operating altitude, cooling conditions, propeller clearance, mission payload, and required power reserve.
Integrated by Design Validated as a System
The motor, ESC, and validated propeller configurations are engineered as one propulsion architecture. This reduces integration work, improves system consistency, and provides a defined starting point for UAV platform development.
Motor and ESC Integration
A compact integrated architecture reduces external wiring, connector count, and installation complexity while supporting more consistent electrical and thermal performance.
Matched Propeller Setup
Propeller sizing is selected around the motor and ESC operating range to balance thrust, efficiency, current draw, and thermal load at the system level.
Faster Platform Integration
A defined propulsion configuration reduces component sourcing, compatibility testing, and repeated tuning during prototype development.
System Level Performance Data
Thrust, efficiency, current, RPM, and temperature are evaluated as a complete propulsion system to support airframe selection and validation.
Built for Reliable Fixed Wing Cruise
Designed for the continuous operating demands of larger fixed-wing and VTOL cruise platforms, with FOC control, shared-airflow thermal management, configurable propeller positioning, and redundant control and monitoring.
FOC Control and Shared Airflow Cooling
FOC control supports smooth and stable power delivery across the cruise operating range. A shared airflow path improves heat dissipation from both the motor and ESC during sustained output.
Adaptive Electronic Propeller Positioning
Configurable electronic positioning holds the propeller at a defined angle after shutdown and automatically adjusts the holding force against incoming airflow. This helps reduce blade-contact risk and supports lower-drag airframe integration.
Redundant Control and Real Time Monitoring
PWM and CAN provide two throttle-input paths for control redundancy. RPM and motor-temperature feedback support real-time propulsion monitoring and fault diagnosis when used with a compatible flight controller.
Secure Propeller and Mounting Interface
Anti-loosening stainless-steel fasteners, anti-slip teeth, and a removable locating pin help resist loosening and shear loads during installation, maintenance, and operation.
Where IV9 Fits Best
IV9 is intended for 28–35 kg fixed-wing and VTOL UAVs that require higher cruise thrust, stable propulsion output, and dependable integration for long-range missions with larger payloads.
Large Area Mapping and LiDAR Surveying
Supports larger fixed-wing and VTOL platforms carrying photogrammetry cameras, LiDAR, multispectral sensors, and heavier survey payloads across wide mission areas.
Long Range Linear Infrastructure Inspection
Suitable for extended inspection routes over transmission lines, pipelines, railways, roads, and coastal corridors, where additional thrust margin supports larger airframes and longer cruise segments.
Remote Area and Emergency Monitoring
Suitable for fixed-wing and VTOL platforms used for disaster assessment, forestry patrol, coastline monitoring, and remote-area observation with heavier sensor or communication payloads.
