With the rapid development of urban air mobility (UAM), manned low-altitude commuting vehicles (e.g., eVTOLs, personal air vehicles) have emerged as a transformative solution for future transportation. Their electric propulsion system (EPS) and onboard auxiliary power distribution, serving as the "heart and arteries" of the entire vehicle, demand extremely high efficiency, power density, and unwavering reliability for critical loads such as propulsion motors, high-voltage battery management, and flight-critical avionics. The selection of power MOSFETs directly determines the system's conversion efficiency, thermal performance, power-to-weight ratio, and operational safety. Addressing the stringent requirements of aerospace-grade safety, peak efficiency, minimal size/weight, and functional integrity, this article centers on scenario-based adaptation to reconstruct the power MOSFET selection logic, providing an optimized solution ready for direct implementation.
I. Core Selection Principles and Scenario Adaptation Logic
Core Selection Principles
High Voltage & Robustness: For propulsion systems operating from 400V to 800V DC bus voltages, MOSFET voltage ratings must withstand significant switching spikes and transients with a safety margin, prioritizing devices with high VDS ratings and avalanche energy capability.
Ultra-Low Loss is Paramount: Prioritize devices with minimal on-state resistance (Rds(on)) and optimized gate charge (Qg) to maximize efficiency, reduce thermal load, and extend flight time/range.
Package & Thermal Excellence: Select packages (TO-247, TO-263, etc.) that offer the best balance of high current capability, low thermal resistance, and weight for forced-air or liquid-cooled heat sinks, crucial for power density.
Aerospace-Grade Reliability: Devices must exhibit exceptional long-term stability under thermal cycling, vibration, and continuous high-load operation, with parameters consistent over the full temperature range.
Scenario Adaptation Logic
Based on the core electrical systems within a commuting vehicle, MOSFET applications are divided into three main scenarios: High-Voltage Propulsion Inverter (Thrust Core), High-Current DC-DC/Power Distribution (Power Management), and Critical System & Auxiliary Control (Safety & Redundancy). Device parameters and characteristics are matched accordingly.
II. MOSFET Selection Solutions by Scenario
Scenario 1: High-Voltage Propulsion Inverter (50kW-200kW+) – Thrust Core Device
Recommended Model: VBP18R35S (Single-N, 800V, 35A, TO-247)
Key Parameter Advantages: Utilizes advanced Super Junction Multi-EPI technology, achieving an Rds(on) as low as 110mΩ at 10V gate drive. The 800V rating provides ample margin for 400V-600V bus systems, handling voltage spikes robustly. The 35A continuous current rating per device enables parallel use for high-power motor phases.
Scenario Adaptation Value: The TO-247 package is ideal for high-power modules with direct thermal interface to cooling systems. Ultra-low conduction loss minimizes heat generation in the inverter, directly improving system efficiency and power density—critical for maximizing payload and range. Its high-voltage capability ensures reliable operation in demanding aerospace environments.
Applicable Scenarios: Phase legs in multi-level or two-level three-phase propulsion motor inverters for eVTOLs and electric aircraft.
Scenario 2: High-Current DC-DC Conversion & Main Power Distribution – Power Management Device
Recommended Model: VBGL11203 (Single-N, 120V, 190A, TO-263)
Key Parameter Advantages: Features SGT technology delivering an exceptionally low Rds(on) of 2.8mΩ at 10V. A massive continuous current rating of 190A supports high-power intermediate bus conversion (e.g., 800V to 48V/28V) and main power distribution with minimal loss.
Scenario Adaptation Value: The D²PAK (TO-263) package offers an excellent balance of current handling, thermal performance, and PCB footprint. Its ultra-low Rds(on) is pivotal for achieving >98% efficiency in non-isolated DC-DC converters and solid-state power controllers (SSPCs), drastically reducing thermal management overhead and weight in the power distribution network.
Applicable Scenarios: Synchronous rectification in high-current DC-DC converters, main battery disconnect switches, and high-current rail distribution boards.
Scenario 3: Critical System & Auxiliary Control – Safety & Redundancy Device
Recommended Model: VBA5101M (Dual N+P, ±100V, 4.6A/-3.4A, SOP8)
Key Parameter Advantages: The SOP8 package integrates a matched pair of 100V N-Channel and P-Channel MOSFETs with good parameter consistency (Rds(on) of 80/150mΩ at 10V). This enables compact, high-side and low-side switch configurations or complementary push-pull designs.
Scenario Adaptation Value: The integrated dual-die configuration saves significant PCB space and simplifies layout for redundant or safety-critical circuits. It is ideal for controlling avionics buses, fan/pump drives, and actuator power where isolated control, fail-safe design, or compact H-bridge configurations are required. The 100V rating suits 48V and 28V vehicle systems.
Applicable Scenarios: Redundant power path switching, avionics load switching, H-bridge drivers for small actuators or valves, and battery management system (BMS) module control.
III. System-Level Design Implementation Points
Drive Circuit Design
VBP18R35S: Requires a dedicated high-speed, high-current gate driver IC with sufficient drive voltage (12-15V recommended) to fully enhance the device and minimize switching loss. Isolated drivers are typically needed for each phase leg.
VBGL11203: Needs a powerful gate driver capable of sourcing/sinking high peak currents to charge/discharge its large gate capacitance quickly. Attention to gate loop inductance is critical.
VBA5101M: Can be driven by lower-current gate drivers or in some cases by MCUs with buffer stages. Proper dead-time insertion is essential for complementary use.
Thermal Management Design
Aggressive Cooling Essential: VBP18R35S and VBGL11203 will be mounted on liquid-cooled or forced-air-cooled heatsinks. Use of thermal interface materials (TIM) with high conductivity is mandatory.
Derating for Altitude & Lifetime: Apply significant current and power derating (e.g., 50% or more of rated current at maximum junction temperature) to ensure lifetime reliability under thermal cycling stress. Junction temperature should be monitored or tightly controlled.
PCB Thermal Design for VBA5101M: Utilize large copper pours and multiple vias to the internal ground/power planes to dissipate heat effectively from the SOP8 package.
EMC and Reliability Assurance
SiN Snubbers and Layout: Use RC snubber networks across the drain-source of high-voltage switches (VBP18R35S) to control dv/dt and reduce EMI. Minimize high di/dt and dv/dt loop areas in PCB layout.
Protection Features: Implement comprehensive desaturation detection, overcurrent protection, and active short-circuit protection for all high-power switches. Use TVS diodes and ferrite beads to protect gate drivers from transients.
Redundancy and Fault Isolation: Design critical power paths (using devices like VBA5101M) with inherent redundancy and fault isolation capabilities, ensuring a single point of failure does not compromise vehicle safety.
IV. Core Value of the Solution and Optimization Suggestions
The power MOSFET selection solution for manned low-altitude commuting vehicles proposed in this article, based on scenario adaptation logic, achieves holistic coverage from the high-voltage propulsion core to intricate power management and safety-critical control. Its core value is mainly reflected in the following three aspects:
Maximized Efficiency for Extended Range: By selecting ultra-low-loss MOSFETs like the SGT-based VBGL11203 and SJ-Multi-EPI based VBP18R35S for the highest power stages, conduction losses are minimized across the powertrain. This directly translates to higher overall system efficiency, reduced battery energy consumption per flight, and ultimately, increased vehicle range and payload capacity—key metrics for commercial viability.
Uncompromising Safety through Intelligent Integration: The use of integrated dual MOSFETs (VBA5101M) and high-reliability discrete devices enables robust, fault-tolerant power architecture design. This supports redundant system design, predictable failure modes, and isolated control of critical functions, forming the hardware foundation for achieving the stringent Functional Safety (e.g., DO-254/DO-178) standards required in aviation.
Optimal Power Density and Cost-Effectiveness Balance: The selected devices represent the optimal point in the performance-cost curve for their voltage classes. Advanced packaging and silicon technologies (SGT, SJ) deliver the necessary power density without resorting to premature adoption of more expensive wide-bandgap (SiC, GaN) solutions in all areas, allowing for a balanced and cost-effective system BOM while meeting performance targets.
In the design of electric propulsion and power systems for manned low-altitude commuting vehicles, power MOSFET selection is a foundational element in achieving the trifecta of efficiency, safety, and power density. The scenario-based selection solution proposed herein, by accurately matching the demanding requirements of different vehicle subsystems and combining it with rigorous system-level design practices, provides a comprehensive, actionable technical reference for aerospace engineering teams. As UAM vehicles evolve towards higher voltages, higher power, and stricter certification, the selection of power devices will increasingly focus on qualification to aerospace standards, model-based reliability prediction, and co-design with cooling systems. Future exploration will inevitably focus on the integration of silicon carbide (SiC) MOSFETs for the highest voltage and frequency stages, and the development of intelligent, monitored power modules, laying the solid hardware foundation for creating the next generation of safe, efficient, and market-ready urban air vehicles. In the dawn of the third dimension in urban transportation, exceptional and reliable power electronics design is the cornerstone of passenger safety and mission success.

Detailed Topology Diagrams