Integrated
Motor Drives for

Electric Aircraft
Electric Boats
E-motorsports
Military & Defense
Power generation
aerospace

Unrivaled power density – 12 kW/kg continuous. The HPDM is the next step in the evolution of electric motor technology.

JOIN THE REVOLUTION.
Patent Pending

250kW in a 16kg Package

The HPDM-250 is an ultra-high power density integrated motor drive for high performance and mass sensitive applications. It combines the electric motor, inverter, and gearbox into a single unit and is the culmination of H3X innovation in multiple areas including:

HPDM-250 Target Specifications

The HPDM-250 is optimized entirely for power density and efficiency. It features the highest level of integration on the market, made possible by our holistic design methodologies rooted in first principles and multidisciplinary expertise in power electronics and electric machines.

Show specs with a 4:1 planetary gearbox
H3X can design a high torque density planetary gearbox that is integrated into the front endcap of the machine to achieve your desired torque-speed requirements. The example 4:1 planetary is based on a real design that is 3 kg and 97% efficient.

These specifications are estimates based on electromagnetic, thermal, and structural simulations. Data from dynamometer will be available early 2022.

Peak Torque
120 Nm at 360 Arms
Peak Power
250 kW
Peak Duration
30 seconds
Speed Range
0 - 20,000 RPM
Continuous Torque
95 Nm
Continuous Power
200 kW
Peak Motor Efficiency
96.7%
Peak Inverter Efficiency
99.0%
Peak Combined Efficiency
95.7%
DC Bus Voltage
Up to 900 V
Mass
13.0 kg
Volume
7.77 L

Motor Torque vs. Speed

Patent Pending

Revolutionizing Winding Technology

H3X has developed a novel stator winding and high voltage insulation system that offers a >40% improvement over conventional windings in terms of maximum continuous current density.

High fill factor (>70%)

Thermally conductive (> 5 W/m-K bulk)

Partial discharge resistant (1800V)

Scalable to higher power MW-class machines

High temperature (265 °C)

Patent Pending

2.8MW in a 220kg Package

12 independent HVDC connectors for fault tolerant independent power delivery chains

12 Independent coolant ports for fault tolerant thermal management.

12 Independent Inverter-Stator sectors for unparalleled fault tolerance.

Hollow shaft for variable pitch mechanism and motor stacking - up to 6 HPDM-3000s (17MW)

The EPU is hermetically sealed front to back to reduce risk of FOD and debris

The HPDM-3000 is an ultra-high power density MW-class Integrated Modular Motor Drive (IMMD) for primary propulsor applications on large electric aircraft. Based on the same core technology as the H3X HPDM-250, this EPU has a continuous specific power of >12 kW/kg and features the highest level of fault tolerance and reliability with its 12 independent drive sectors.

Stackable up to 17MW for large commercial electric aircraft

Specifications:
Max Continuous Power
2.8 MW
Max Continuous Torque
16,000 Nm
Mass
220 kg
Max Speed
1667 RPM
Efficiency at Cruise (typical)
94%
Sector Voltages
600 – 900 VDC
DC Input Voltage
Up to 4.8kV
Max Operating Altitude
45,000 ft
Diameter
3 ft
Length
1 ft
# of Independent Sectors
12
Communication Protocols
CAN x12, RS485 x12
Time Between Overhaul
10,000 hours
FAA Certification Intent
DO-160G, DO-178C, DO-254

These specifications and curves are estimates based on electromagnetic, thermal, and structural FEA simulations

Specifications:
Max Continuous Power
5.6 MW
Max Continuous Torque
32,000 Nm
Mass
440 kg
Max Speed
1667 RPM
Efficiency at Cruise (typical)
94%
Sector Voltages
600 – 900 VDC
DC Input Voltage
Up to 4.8kV
Max Operating Altitude
45,000 ft
Diameter
3 ft
Length
2 ft
# of Independent Sectors
24
Communication Protocols
CAN x12, RS485 x12
Time Between Overhaul
10,000 hours
FAA Certification Intent
DO-160G, DO-178C, DO-254

These specifications and curves are estimates based on electromagnetic, thermal, and structural FEA simulations

Specifications:
Max Continuous Power
8.4 MW
Max Continuous Torque
48,000 Nm
Mass
660 kg
Max Speed
1667 RPM
Efficiency at Cruise (typical)
94%
Sector Voltages
600 – 900 VDC
DC Input Voltage
Up to 4.8kV
Max Operating Altitude
45,000 ft
Diameter
3 ft
Length
3 ft
# of Independent Sectors
36
Communication Protocols
CAN x12, RS485 x12
Time Between Overhaul
10,000 hours
FAA Certification Intent
DO-160G, DO-178C, DO-254

These specifications and curves are estimates based on electromagnetic, thermal, and structural FEA simulations

Specifications:
Max Continuous Power
11.2 MW
Max Continuous Torque
64,000 Nm
Mass
880 kg
Max Speed
1667 RPM
Efficiency at Cruise (typical)
94%
Sector Voltages
600 – 900 VDC
DC Input Voltage
Up to 4.8kV
Max Operating Altitude
45,000 ft
Diameter
3 ft
Length
4 ft
# of Independent Sectors
48
Communication Protocols
CAN x12, RS485 x12
Time Between Overhaul
10,000 hours
FAA Certification Intent
DO-160G, DO-178C, DO-254

These specifications and curves are estimates based on electromagnetic, thermal, and structural FEA simulations

Specifications:
Max Continuous Power
14 MW
Max Continuous Torque
80,000 Nm
Mass
1100 kg
Max Speed
1667 RPM
Efficiency at Cruise (typical)
94%
Sector Voltages
600 – 900 VDC
DC Input Voltage
Up to 4.8kV
Max Operating Altitude
45,000 ft
Diameter
3 ft
Length
5 ft
# of Independent Sectors
60
Communication Protocols
CAN x12, RS485 x12
Time Between Overhaul
10,000 hours
FAA Certification Intent
DO-160G, DO-178C, DO-254

These specifications and curves are estimates based on electromagnetic, thermal, and structural FEA simulations

Specifications:
Max Continuous Power
16.8 MW
Max Continuous Torque
96,000 Nm
Mass
1320 kg
Max Speed
1667 RPM
Efficiency at Cruise (typical)
94%
Sector Voltages
600 – 900 VDC
DC Input Voltage
Up to 4.8kV
Max Operating Altitude
45,000 ft
Diameter
3 ft
Length
6 ft
# of Independent Sectors
72
Communication Protocols
CAN x12, RS485 x12
Time Between Overhaul
10,000 hours
FAA Certification Intent
DO-160G, DO-178C, DO-254

These specifications and curves are estimates based on electromagnetic, thermal, and structural FEA simulations

The HPDM-3000 is the culmination of H3X innovation in electric machines, power electronics, material science, control systems, and advanced manufacturing.

Who We Are

A team of multidisciplinary engineers brought together with the sole purpose of developing the most advanced electric aircraft propulsion systems in the world to enable sustainable aviation.

Why did we start H3X?

For electric aircraft to be commercially feasible, substantial improvements need to be made to electric propulsion system technology.  Today, best-in-class motors and inverters have a combined power density of 3-4 kW/kg.  ARPA-E has determined that for a Boeing 737 to complete a typical five hour flight, the propulsion system must be >12 kW/kg continuous.

We have the solution.

At 12 kW/kg continuous, the HPDM exceeds ARPA-E’s requirements and is at least 3X better than current systems. It is a step change in electric propulsion technology and removes one of the main barriers blocking widespread commercialization of electric aircraft.

Where can the HPDM products be used?

Any mass-sensitive, packaging-constrained, or high performance application.

HPDM-250 applications: eVTOL urban air mobility, military aircraft and vessels, electric boats, e-racing, power generation

HPDM-3000 applications: Large commercial electrified aircraft, electric ships and ferries, power generation

Our Investors

H3X Founders

H3X brings together driven minds from the automotive, aerospace, and motorsports industries with deep knowledge in electric motors, power electronics, & vehicle engineering. We love what we do and are looking to hire people who share that same passion.

As CEO, Jason is responsible for overall business direction and power electronics development at H3X.  His speciality lies at the intersection of business leadership and hardcore engineering. Prior to H3X, he started his own engineering consulting company where he has helped several companies in the automotive and aerospace industries bring their EV product visions to life.  He has a B.S. and M.S. in Electrical Engineering from University of Wisconsin-Madison. Fun fact - Jason (and Max) co-founded UW-Madison’s electric Formula SAE team and built the first AWD electric racecar in the United States.

Jason Sylvestre

Chief Executive Officer

Max is a multidisciplinary engineer with a laser focus on physics fundamentals and deep knowledge in both mechanical and electrical engineering. As CTO, he is responsible for H3X’s overall product engineering, electric motor design, and core technology development. Max’s background includes holding key roles in vehicle modeling, architecture, and electric motor design in both the automotive and aerospace sectors. He has a B.S. in Mechanical Engineering and an M.S. in Electrical Engineering from University of Wisconsin-Madison.

Max Liben

Chief Technology Officer

Eric is responsible for all operations and mechanical design at H3X. In Eric’s prior roles, he has lead projects to develop control systems for electric and hybrid powertrain systems from the ground up. He has a B.S. in Mechanical Engineering from University of Wisconsin-Madison. Eric comes from a proud heritage of craftsmen – from butchers and bakers to electricians and steamfitters. This unique background has enabled to him bridge the gap between advanced engineering theory to practical and scalable solutions.

Eric Maciolek

Chief Operating Officer

Latest Media

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Get in Touch

Contact H3X today to see how you can use our products in your vehicles. We are looking to develop long-term relationships with first adopters and partners interested in revolutionizing the aircraft industry and creating a sustainable future.


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Designed and Made in the United States of America

Designed and Made in the United States of America

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