950KV
3220 · 6SHigh response
Developed for interceptor and FPV-class applications.
Midguard 3220
Midguard 3220 BLDC drone motor platform
A pre-production 6S outrunner platform for European UAV manufacturers, with 700 KV and 950 KV development variants.
MG-3220Pre-production
- Platform
- Midguard 3220
- Motor type
- Outrunner BLDC
- Battery architecture
- 6S
- Development variants
- 700 KV · 950 KV
- Status
- Pre-production
- Engineering & prototyping
- Vaasa, Finland
Platform facts reflect the current development configuration. Configuration-specific performance data is shared with qualified OEM partners.
Development variants
Two KV variants on one mechanical and electromagnetic platform
Both variants share the 3220 outrunner architecture and 6S battery configuration. The KV rating positions each variant for a different UAV duty profile.
700KV
3220 · 6SEndurance
Developed for endurance-focused applications where lower KV and efficient operation are priorities.
Final performance depends on the complete propulsion setup, including propeller, ESC, voltage, cooling and duty cycle. Configuration-specific test data is available to qualified OEM partners.
Application positioning
Matched to the duty profile, not to a marketing category
Motor performance cannot be separated from battery voltage, propeller, ESC, cooling and duty cycle. Midguard therefore works with OEMs at system level and provides configuration-specific data and recommendations.
- 950 KV
High-response applications
Positioned for interceptor and FPV-class platforms where rapid throttle response and acceleration dominate the duty profile.
- 700 KV
Endurance applications
Positioned for endurance-focused platforms where lower KV and efficient operation across long, steady segments are the priority.
Development status
Current phase: pre-production and industrialisation
- Current phase
- Pre-production and industrialisation
- Available activities
- Requirements review, sample evaluation and qualification planning
- Sample availability
- Contact us for current availability
Prototype built & tested
CompleteOEM evaluation
CurrentPilot manufacturing
NextRepeatable scale
Future
Published pre-production test summary
Current evaluation data — not a product specification
The figures below are taken from the public product overview of September 2026. They describe one pre-production evaluation setup. Peak values should not be interpreted as one simultaneous operating point or a continuous rating.
- Motor mass
- ≈ 160 g
- Peak electrical input
- 2.14 kW
- Peak observed thrust
- ≈ 5.5 kgf
- Test configuration
- 6S
Pre-production unit as measured in the published overview.
Electrical input power, not shaft output power.
Highest thrust observed in testing.
Current 6S setup with 700 KV and 950 KV pre-production variants.
- Peak values should not be interpreted as one simultaneous operating point or a continuous rating.
- The figures apply to the tested pre-production configuration and propeller only. They do not describe every variant, propeller or duty profile.
- Bench testing was carried out independently at OAMK in June 2026. Results are current evaluation data, not a guaranteed or certified specification.
- Achievable performance depends on the battery, propeller, ESC, cooling, duty cycle and overall configuration of the platform.
Sourcing approach
Sourcing defined at motor level
Final assembly in Europe is not enough if critical motor components still depend on one supply region. The 3220 was designed so that magnet and component configuration can follow the OEM program’s continuity requirements.
- 01
Developed from scratch to support European-sourced rare-earth magnet configurations and reduce dependence on a single supply region.
- 02
Component strategy is defined per OEM program against a specific product configuration, so sourcing statements can be traced to the bill of materials.
- 03
Repeatable pilot production is being prepared in Finland alongside the current OEM evaluation phase.
OEM engagement
How an evaluation program runs
- 01
Define requirements
Requirements cover operating profile, voltage, propeller envelope, environment, compliance needs and volume.
- 02
Configure the motor
A 3220 variant and component configuration are proposed against the defined requirements.
- 03
Test and qualify
Samples are evaluated on the bench and in the OEM’s own setup, with a qualification plan agreed together.
- 04
Pilot production
Repeatable pilot batches are produced in Finland once the configuration is frozen.
- 05
Scale
Volume ramp is planned against demonstrated pilot output and the program’s own timeline.
Next step
Request configuration-specific technical data
Share your platform, operating profile and expected volumes. We respond with the relevant 3220 variant, configuration recommendations and the current sample situation.