The FlySpark HERO VTOL Drone is a next-generation vertical take-off and landing (VTOL) fixed-wing UAV engineered for professional mapping, surveying, and monitoring applications.
Constructed with a lightweight and durable blend of EPO foam, carbon fiber, aviation-grade aluminum alloy, and engineering plastics, the HERO VTOL delivers the perfect balance between strength, stability, and flight endurance.
Featuring an advanced aerodynamic design with a high-efficiency V-tail structure, optimized wing and fuselage integration, and a streamlined body, this UAV minimizes drag while maximizing lift and flight performance.
The HERO VTOL drone ensures exceptional flight stability, efficient cruising speeds, and long-endurance performance—ideal for topographic mapping, agricultural monitoring, infrastructure inspection, and environmental surveys.
✅ Key Highlights
Vertical Takeoff and Landing (VTOL): Eliminates runway dependency, enabling operation in limited or rugged areas.
Extended Endurance: Up to 136 minutes / 144 km flight range with mapping configuration.
Precision Aerodynamics: Optimized lift-to-drag ratio ensures stable long-distance flight at speeds of 17–22 m/s.
Lightweight & Durable Frame: Built from EPO foam + carbon fiber + aluminum alloy for strength with minimal weight.
Quick Disassembly: Tool-free quick-release structure for fast deployment and transport.
Adaptable Mission Use: Supports payloads up to 1 kg, suitable for cameras, LiDAR, or sensors.
High Altitude Capability: Operates reliably at up to 6,500m ceiling altitude with wind resistance up to Level 5.
Dual Endurance Modes: Optimized flight times for mapping (136min) and monitoring (125min) tasks.
Technical Specifications
Aerial Platform
| Item | Specification |
|---|---|
| Material | EPO, Carbon Fiber, Aviation Aluminum Alloy, Engineering Plastic |
| Wingspan | 2180 mm |
| Vertical Arm | 755 mm (with motor base) |
| Wing Area | 53 dm² |
| Body Length | 1140 mm |
| Body Height | 255 mm (with tripod) |
| Wing Mounting Angle | 2.9° |
| Aircraft Angle of Attack | 0–2° |
| V-Tail Angle | 28° up / 20° down |
| Takeoff Method | Vertical Takeoff and Landing |
| Takeoff Weight | 7 kg |
| Payload | 1 kg |
| Ceiling Altitude | 6500 m |
| Takeoff Altitude | ≤3000 m |
| Wind Resistance | Level 5 |
| Operating Temperature | -10°C to 50°C |
| Packing Box Size | 1100 × 350 × 430 mm |
| Disassembly | Tool-free Quick Release |
⚙️ Flight Performance
| Parameter | Value |
|---|---|
| Cruising Speed | 17–22 m/s |
| Stall Airspeed | 12 m/s |
| Conversion Airspeed | 14 m/s |
| Max Climb Angle | 3.5° |
| Max Dive Angle | 5° |
| Max Roll Angle | 30° |
| Mapping Endurance | 136 min / 144 km (19 m/s, 600g payload, 6S@22000mAh battery, 6.65kg TOW) |
| Monitoring Endurance | 125 min / 126 km (18 m/s, 450g payload, 6S@22000mAh battery, 6.5kg TOW) |
Design & Aerodynamics
Streamlined Airframe: Reduces drag and improves lift efficiency.
Optimized Wing-Fuselage Integration: Enhances load distribution and flight balance.
V-Shaped Tail: Improves aerodynamic stability and control precision.
Advanced Lift Distribution: Achieves high flight efficiency and smooth cruising performance.
⚙️ Assembly & Compatibility
Quick disassembly and assembly without tools.
Supports a wide range of mapping payloads, cameras, and sensors.
Includes assembly instructions and user manual download links for setup support.
⚠️ Notes
If unable to order directly via website, contact the FlySpark Sales Team for personalized support.
Production Lead Time: 7–10 working days (depending on customization).
Shipping Duration: 7–14 additional days.
Product upgrades include enhanced aerodynamic tuning and improved V-tail control performance.
The Hero VTOL drone adopts a high-efficiency V-shaped tail, and at the same time optimizesthe aerodynamic shape and relative position of the wing, tail and fuselage. The aerodynamic load distribution is reasonable, the lift and drag are significantly increased, andthe flight efficiency is high.
The Hero VTOL drone adopts a streamlined shape as a whole to reduce flight resistance asmuch as possible while ensuring stable flight.
BOM/WIRING
A large number of high-strengthand light-weight carbon fibers,wooden boards and PC boardsare used in the materials.
In terms of shape, a largenumber of embedded boxstructures are used to com-prehensively improve thestructural strength and rigidi-ty of the body.
On the basis of the “over-load experiment”,accordingto the structural form andload characteristics of thewing, tail and fuselage, thestructure is optimized ac-cording to the gram preci-sion to minimize unneces-sary weight.
Hero VTOL drone supports a variety of loads, covering two application scenarios of mappingand monitoring.
The wing and tail adopt a tool-free quick disassembly structure, which reduces theinstallation steps and shortens the disassembly time.
The inner liner of the packing box is made of high-rate EPS foam, with light specificgravity, good impact resistance and shock resistance, and is suitable for long-dis-tance transportation.
The bottom of the fuselageadopts the rear three-pointlanding gear, with high groundclearance, large mountingspace, and the tail rotor doesnot touch the ground.
Aircraft center of gravitybulges under fuselagehooks and wing root plasticstart (same location).
The inner side of the fuselageis designed with wire groovesand removable baffles to fa-cilitate the installation ofwires, and the wiring in thecabin is simple and efficient.
The nose cabin adopts afour-point connection struc-ture, which is stable and reli-able and supports quick re-lease.
Two 9-pin connectors are re-served in the nose cabin tosupport the connection ofsignals such as image trans-mission, remote control, andairspeed to the fuselage flightcontrol.
The design file of the nosecabin is open source, and userscan customize the mountingplate according to the installa-tion hole position of the pod.
The size of the battery compart-mentis 326*110*78mm,and themaximum support is6S@30000mah solid-state lithi-um battery.
The battery holder is CNC ma-chined from PC board, which islight in weight and has goodimpact resistance.
The battery tie is made of fi-ber-reinforced plastic, which isstrong and durable. The layoutof the tie is reasonable andeasy to fix.
The flight control cabin adoptsa layered design structure toimprove space utilization. Thebottom layer can install thedistribution board and thelanding radar.
The size of the payload bay is 144*160*80mm, which can accommodate Sony A7R seriescameras or five-lens half-frame tilt cameras.
The middle layer can instalflight control, which is compat-ible with open source/com-mercial flight control installa-tion.
The top layer can install PPK orimage transmission equipment.
The flight control hatch sup-ports screw fixing to preventforeign objects from fallingwhich is both beautiful anddust-proof.
The GPS and compass modulesare placed above and behindthe flight control cabin, andthe electromagnetic environ-ment is clean.
The position of the PPK anten.na is reserved behind the GPScabin, which is convenient toinstall the PPK antenna andimprove the accuracy of POSdata.
The tail push ESC is placedunder the rear of the flightcontrol cabin, with an exter-nal aluminum shell, which hasa good heat dissipation effect.
The 195mm rat tail glue stickantenna can be pre-buried inthe vertical tail, which notonly improves the supportstrength of the vertical tail,but also has a clean electro-magnetic environment and
The V-tail adopts a tool-freequick-release structure, whichis automatically locked withone push and pulled out im-mediately with one push.
The tail servo does not needto be pre-embedded for easymaintenance.
The servo rocker arm is designed with built-in, even ifthe rocker arm drive columnis loose, the rudder surfacecan be accurately executed.
The wing can be split into awing root segment and a wingtip segment to further reducethe storage volume.
The wing is composed of maincarbon tubes, auxiliary carbontubes, vertical arms, and plas-tic parts to form a framestructure to improve the over-all strength.
The wing root section and thefuselage are separated electri.cally and structurally through5+2 high-current connectors.
The surface of the wing rootsection is reinforced with 3Mstickers, which enhances therigidity of the aircraft and im-proves the torsion resistanceof the wing.
The wing rudder adopts servorocker arm direct drivedesign, simple and durable
The VTOL Rotor Arm is fixedby an aluminum alloy wrap-ping structure, which can beinstalled and removed as awhole for easy maintenance.
The middle section of theVTOL Rotor Arm is open to fa-cilitate the installation of ESCand servo cables.
(Optional) Wiring boardQuick-release wing powersystem
The motor seat supports thelargest outer rotor ф65mmmotor, and the size of the ESCcabin is 67*31*12mm
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