Propulsion
H15 MD PLUS COAXIAL DRIVE
- Motor
- 15635 / 31KV
- ESC
- 300A 24S FOC
- Propeller
- MSC 72×25 carbon
- Rated thrust
- 45 kg per axis
- Max thrust
- 110 kg+ per axis
Verified Physical PrototypeTHE FUTURE OF
THE FUTURE OF
HEAVY-LIFT AERO.
Defense logistics and urban air mobility, powered by solid-state batteries and coaxial industrial propulsion.
Current Lift CapVerified
800KG
ALUMINUM CHASSISPHASE 01
Propulsion
Coaxial
Dual counter-rotating motors per arm for thrust density and redundancy.
Power
28S HV
~115 V nominal to cut I²R losses and wiring weight.
Energy
Solid-State
Puncture-proof cells, immune to thermal runaway, high energy density.
Scalability
1,500 KG
Modular architecture upgrades to heavy industrial motors.
THE HIGH-RISK PHASE IS ALREADY BEHIND US
A complete physical prototype exists today on an optimized aluminum chassis. System architecture, coaxial propulsion and power distribution are built and verified in practice.
Capital goes to a carbon-fiber airframe and certification — not to uncertain baseline research.
Real footage — not a render
FROM THE FACTORY FLOOR
Unedited workshop footage of the current aluminum prototype being built — no CGI, no animation, no post-production. Same aircraft as in the prospectus: coaxial rotor arms, high-voltage battery modules, hardwired cockpit controls. Formal flight and safety evaluations are the next roadmap phase.
STAGE
IN ASSEMBLY
AIRFRAME
ALUMINUM / PHASE 01
SOURCE
RAW CAPTURE
CGI
NONE
Unedited · Filmed on site
CORE HARDWARE
Industrial components / integrated in-house
Energy
SOLID-STATE BATTERY MODULE
- Capacity
- 91,000 mAh
- Discharge
- 5C
- Chemistry
- Solid-state
- Pack
- 12S/14S → 24S–28S
- Bus
- ~100–115 V nominal
Ground Support
2,800 W DUAL-CHANNEL CHARGER
- Charge power
- 2,800 W
- Output
- 2 × 1,400 W (AC 220V)
- Charge current
- 10 / 15 / 20 / 25 / 28 A
- Cell count
- 6–14S
- Weight
- 7.4 kg
Command & Control
SIYI UniRC 7PRO GROUND STATION
- Range
- Up to 40 km
- Software
- QGroundControl / UniGCS
- Operators
- Dual, with takeover
- Link
- Full-frequency RTK
- Telemetry
- MAVLink
180 kg recommended takeoff weight (4 axes / 8 props) · up to 100 kg payload · 100 V / 28S · components rated −40 to 65 °C · ~15% lower current draw than 24S.
ZERO SINGLE POINT OF FAILURE
Three-Tier Failsafe Matrix Protocol
Tier 01 / Signal
Hardwired Cockpit Priority
A mechanically mounted joystick bypasses all wireless latency through a PWM to CAN/SBUS hardware converter for absolute signal integrity.
Tier 02 / Logic
Triple-Redundant IMU
The VK V10 PRO autopilot runs triple-redundant IMUs and GNSS receivers. A physical red emergency button locks the aircraft into self-stabilizing hover.
Tier 03 / Kinetic
Ballistic Recovery
Rocket-actuated parachute deployment triggers Gigavac isolation, killing all 100V power in milliseconds while the 12V UPS keeps telemetry and GPS active.
THREE CAPITALIZED MARKETS
One core architecture — VK V10 PRO + SIYI GCS
Vertical A
Defense Logistics
Autonomous resupply of 460–1,500 kg to the front line — no crew on the high-risk last mile.
Vertical B
Urban Air Taxi
Redundant passenger and baggage transport between city hubs, above ground congestion.
Vertical C
Industry & Emergency
Heavy lift into inaccessible terrain, plus wildfire and flood disaster relief.
INVESTMENT ALLOCATION
From a working aluminum prototype to a certified commercial product line.
Request Data Room AccessPHASE 01: Material Optimization
Transition from the aluminum chassis to a full-scale carbon-fiber frame, reducing airframe weight by up to 40% and extending range and duration.
PHASE 02: System Refinement
Finalizing BMS integration for real-time solid-state cell health and diagnostic streaming to the SIYI ground control interface.
PHASE 03: Certification Process
Initiating formal flight and safety evaluation programs with aviation authorities, based on the three-tier failsafe architecture.
PRE-ORDER & INFORMATION
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