Acecore Neo Octocopter
Product descripton: Acecore Neo Octocopter by Acecore Technologies
The NEO is a lightweight multipurpose Remotely Operated Aerial Vehicle for commercial use. Its eight-rotor supported frame allows the Pilot in Command to use it for a wide range of missions in various weather conditions.
Custom-designed brushless motors increase redundancy and provide strong resistance to wind gusts and high payloads. Flexible battery mounting enables quick payload changes. With a maximum take-off mass of 19 kg, the NEO is built for operators with the highest demands.
General Features
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Robust carbon fiber frame
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Up to 9 kg useful payload
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All-weatherproof design
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500 m / 5 km / 16 km range options
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Single or dual operator setup
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ADS-B ready transponder
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AES-128 encrypted radio link
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Triple redundant autopilot
Technical specifications
Weights
| Parameter | Value |
|---|---|
| Maximum takeoff mass | 19 kg / 41.89 lbs |
| Maximum payload | 9 kg / 19.84 lbs |
| Minimum standard empty weight | 7.3 kg / 16.09 lbs |
Drive System
| Parameter | Value |
|---|---|
| Energy type | Electrical |
| Number of motors | 8 |
| Motor type | Direct drive 3-phase BLDC outrunner |
| Operating voltage | 25 V |
| Motor max continuous power | 900 W |
| Idle speed | 450 RPM/V |
| Number of ESCs | 8 |
| Max continuous current draw | 60 A |
Propellers
| Parameter | Value |
|---|---|
| Material | Carbon Fiber Reinforced Plastic (CFRP), foamed core, 3K twill weave |
| Propeller setup | 4 CW + 4 CCW |
| Propeller type | 18 × 6.5 inch fixed |
Payload Integration
| Parameter | Value |
|---|---|
| Vibration isolation | Octo metal wire damper system |
| Mounting options | Top and bottom |
| Mounting system | User preference |
| Battery rack position | Top of centerpiece or bottom quick-release |
Avionics
| Parameter | Value |
|---|---|
| Flight controller | Cube |
| Versions | Orange / Blue |
| Operating temperature | −40°C to +85°C (−40°F to +185°F) |
Battery System
| Parameter | Value |
|---|---|
| Energy type | Electrical |
| Battery type | Lithium Polymer |
| Recommended batteries | Tattu 4500 / 10000 / 17000 / 23000 mAh |
| Nominal voltage | 22.2 V (6S) |
| Minimum quantity | 2 packs (parallel) |
| Maximum voltage | 25.2 V |
| Minimum average voltage | 21.0 V |
Dimensions
| Parameter | Value |
|---|---|
| Frame dimensions (L×W×H) | 910 × 910 × 635 mm |
| Rotor-to-rotor diagonal | 1260 mm |
| Diameter with propellers | 1605 mm |
| Height to payload quick release | 480 mm |
| Ground clearance (top propeller) | 650 mm |
| Ground clearance (bottom propeller) | 500 mm |
Weather Limitations
| Parameter | Value |
|---|---|
| Max operating temperature | +50°C |
| Min operating temperature | −15°C |
| Max flight endurance | 25 min |
| Max wind speed | 35 knots |
| Max wind gusts | 40 knots |
| Precipitation | Moderate rain (dry conditions recommended) |
| Max rainfall | 10 mm/h, 30 mm / 3 h |
Flight Limitations
| Parameter | Value |
|---|---|
| Max pitch / roll | 45° |
| Max yaw rate | 150° / s |
| Max flight speed | 91 km/h (horizontal) |
| Flight modes | GPS, Attitude, Auto, Brake, Stabilize |
| Typical ascent | 5 m/s |
| Typical descent | 4 m/s |
| Hover accuracy | Vertical ±0.05 m / Horizontal ±0.05 m |
| RTL cruise speed | 3–9 m/s (variable) |
Accessories
The Acecore NEO supports a wide range of accessories for control, transport, and mission configuration. Payloads are configured independently of the platform.