H6 Hybrid

Carrier H6 Hybrid EFI

Revolutionizing Aerial Power

The Carrier H6 Hybrid EFI (Electronic Fuel Injection) is a multi-hour, high-endurance hexacopter powered by a 2-stroke gasoline generator. The H6 EFI platform offers payload versatility for a wide variety of long duration mission profiles. This system comes ready to plug-and-play to any of the three compatible power formats provided by Harris Aerial.

The Carrier H6 Hybrid’s airframe is fully convertible to hydrogen-electric (Carrier H6 Hydrone), or fully electric (Carrier H6 Electric).  The H6 is the only aircraft in the world that has three power formats, all of which take just minutes in conversion times.

The Carrier H6 Hybrid HE+ is equipped with the H2400EFI generator providing 2400W of continuous power. The system can fly for up to 2.5 hours with a 5kg payload.. 

The system is popular for many applications including but not limited to: LiDAR surveying, photogrammetry, utility inspections, large corridor mapping, surveillance, and many more.

Features

Adaptable, Powerful, Versatile

Easy Mission Planning

Intuitive GCS Telemetry

Transform Your Aerial Operations

Upgrade to the H6 Hybrid Carrier for unmatched flight endurance and efficiency. Experience hybrid-powered performance with extended flight times and superior payload capacity. 

Applications

Explore the Diverse Possibilities

Specifications

Performance Meets Versatility

The Carrier H6 Hybrid EFI (H6EFI) is equipped with an electronic-fuel injection generator yielding 2.4kw continuous power.

H6 Hybrid EFI (H6EFI)

  • Max Payload: 5kg
  • Diagonal Wheelbase 1590 mm
  • Folded Diagonal Wheelbase 658 mm
  • Propeller Size 29"
  • All-Up Weight (No Payload): 14.5kg (No Fuel) / 16.5kg (With 2.5L Fuel)
  • Max Take-Off Weight 23 kg
  • Speed 15 m/s
  • Flight Time: 3 hours (4L Fuel)
  • Max Flight Time 5 hours
  • Voltage 48 V
  • Fuel Capacity 6.5L

Powerplant

  • Engine Model H2400 EFI (Electronic Fuel Injection) Generator
  • Max Continuous Power 2.4 kw
  • Max Instantaneous Power 8 kv
  • Auxiliary Power 5.3 V, 12 V , 24 V, 48 V Power Ports
  • Safety Features - Engine Temperatur Monitoring
    - Throttle % Monitoring
    - Active Engine RPM Feedback
  • Engine Mode Status Stop | Idle | Run
  • Fuel Monitoring - Real-Time Fuel Flow Sensing via EFI
    - Engine Run Time Calculator
  • Fuel Type Unleaded 93 Octane

Operation and Environmental

  • Operation Temp -20 C to 40 C | -4 F to 104 F
  • Max Operational Wind Speed 25mp | 11 m/s
  • Service Ceiling AMSL 6560 ft | 2000 m (Payload Dependant)
  • Service Ceiling AGL 400 ft | 122 m (FAA Limited)

Motors and Propellers

  • # Motors 6
  • Equivalent KV KV100 Motors
  • Optimal RPM 2200 - 2800 RPM
  • Motor Configuration HEXA X
  • Propeller Material Carbon Fiber with Aluminum Hub
  • Propeller Dimensions 29.2 in x 9.2 in

Command and Control

  • Harris C-GCS -19 in Dual HD Display
    - Hands-on Throttle-and-Stick (HOTAS)
    - Freq: 902 - 928 MHz
    - 12 Channel Functionality
  • hereLink - Handheld Remote
    - 5.5 in Display
    - Freq: 2.4 GHz (ISM)
    - 32 Channels Functionality
    - NDAA Compliant

Flight Controller

  • Flight Controller Cube Orange
  • Data Transmission Range 12.5 mi | 20 km (Ideal Conditions)
  • Firmware Custom ArduPilot
  • Takeoff and Landing Autonomous or Manual Control
  • Flight Tracking ADS-B (Receiver)
  • Safety Features - Triple Redundant IMU
    - Redundant Power Supply

Battery

  • Battery Type 6s2p LIPo (2x Batteries)
  • Peak Battery Voltage 50.4 V
  • Nominal Battery Voltage 44.4 V
  • Battery Capacity 5000 mAh
  • Battery Life Cycle 250 Flights
  • Battery Connector XT90-S (Anti-Spark)

H2400 EFI Generator​

Specifications

  • Weight 3.8 kg without accessories / 4.8 kg total
  • Total Power 2.4 kW continuous
  • Dimensions(L x W x H) 355 x 319 x 251 mm
  • Output voltage DC 12 S (49V)
  • Fuel consumption: 750 g/ kw·h(hovering 2.5 Liter/hour
  • Service Temperature: -20 ~ 40 °C / -4 ~ 104
  • Altitude (above sea): 3000 m
  • Fuel High octane #93 or above gasoline

View the H6 Hybrid brochures

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