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Engineering Deep Dive

Platform
Technology

The design is built around a simple idea: keep the important parts fixed, and make the rest easy to swap when the job changes.

Core Architecture

Persistent Core

This is the part that stays the same from one mission to the next: flight control, power, computing, heat handling, and communication.

STRUCTURE
Load-Bearing Carbon Fiber
It is not just a box for parts. The core also carries loads and helps the wing structure stay strong under stress.
6gUltimate Load
3gOperational
15%Safety Margin
COMPUTING
Integrated Intelligence
The flight controller, onboard processor, power system, cooling, and communications all live in the same core so the aircraft stays dependable.
PRODUCTION
Mass Production Ready
The same core can be used across versions, while wings and payload pieces can be changed as needed without reworking the whole aircraft.
REPAIR
Field Maintainable
It is meant to last and to be repaired in the field. A single technician can make a configuration change without a long setup process.
10yrService Life
1Technician
Mission Interface

QRAM System

The QRAM system is the connection point between the core and the parts that change with each mission. It is built to be swapped out quickly without needing a lot of setup.

MECHANICAL
Tool-Free Interface
The interface uses simple mechanical alignment so the parts lock in place cleanly and stay secure when mounted.
ELECTRICAL
48V Power Bus
The power connection is simple and robust, with protection built in so it can be changed over without much trouble.
DATA
Gigabit + CAN Bus
The system carries data and control signals in a simple way so the aircraft can recognize each wing setup and adapt without a manual reset.
PNEUMATIC
Mission-Ready Interface
The core keeps the lifting system intact even when the wings change, so the aircraft does not lose its basic VTOL capability during a swap.
<3minFull Swap
6Wing Configs
Validated Swap Timeline
Wing Release
0:15
Payload Swap
0:45
Wing Attach
0:30
System Check
0:30
Pre-Flight
0:40

TARGET: <3:00 TOTAL · SINGLE TECHNICIAN · NO TOOLS REQUIRED

Propulsion Architecture

Coaxial Propulsion

The propulsion setup is built to be simple and useful. It can lift the aircraft directly, then shift into forward flight without a lot of extra hardware.

01°
Coaxial Counter-Rotating Drive
Two motors spin in opposite directions so the aircraft can keep its balance without relying on a tail rotor or extra balancing hardware.
02⟳
Variable-Pitch Propellers
The propellers can change their pitch to suit hover or cruise, which helps the aircraft stay efficient in both modes.
03↑
Vertical Launch Sequence
The system can lift the aircraft straight up first, then gradually move into forward flight once the aircraft has enough speed.
04↓
Controlled Vertical Landing
It can keep its hover ability during descent, which makes landing in uneven places more practical.
05⟲
Hover Stabilization
The airflow from the propellers helps with stability while the aircraft is hovering, especially in gusty conditions.
06⚡
Transition Control
The aircraft shifts smoothly between lift-based control and wing-based control as it moves between hover and cruise.
Propulsion Specifications
ParameterHover / VTOLCruiseNotes
Drive configurationCoaxial, Counter-RotatingSameSingle thrust axis
Propeller diameter30–36"30–36"Variable-pitch carbon
Peak power draw4–6 kW600–900 WClimb: 1.5–2.5 kW
Battery voltage12S–14SSameHigh-density Li-ion
Gimbal pitch authority±15° to ±25°NeutralHover & transition control
Gimbal yaw authority±10° to ±15°NeutralHover directional control
Minimum hover thrust>1.3× MTOW—Stable ascent margin
Power Architecture

Energy & Solar Systems

The wings can help capture energy from the sun, which supports longer flights during the day and gives the aircraft a backup for the night.

PHANTOM Logo
Phantom Power Budget
Peak Solar Output 600W
Realistic Average (80%) 480W
Cruise Load 230W
Daylight Surplus +250W
Battery Capacity 222 Wh
Night Reserve 46 min
Daylight Endurance ∞
Battery Technology Roadmap

From Storage to Structure

2024
NMC 811 Lithium-Ion
A simple battery module that gives the aircraft a practical energy reserve.
222 Wh Capacity
2026
Solid-State Lithium
A lighter and more efficient option that still fits the aircraft layout.
300 Wh Capacity
2028
Semi-Structural Battery
A version that begins to share some of the wing structure instead of sitting as a separate block.
350 Wh Effective Wh/kg
2030
Full Structural Battery Wing
A more ambitious future version where the wing structure itself helps store energy.
420 Wh Structural Wh
Structural Analysis

Load Paths
& Margins

The wing and its mounting system are designed to stay strong through repeated use and to handle the loads that come with real flying.

Load CaseLimit LoadUltimate Load (1.5×)Status
2.5g level flightDesign cruise3.75g✓ PASS
3.0g pull-up maneuverOperational limit4.5g✓ PASS
Vertical gust (15 m/s)Structural limit—✓ PASS
Landing ground loads2× landing weight3×✓ PASS
Torsional QRAM load500 N·m750 N·m✓ PASS
Ultimate load factor4g6g✓ PASS (+15% margin)
DEFLECTION
Wing Tip Limits
The wing stays within safe limits under normal use, and it is built to avoid instability even when things get rough.
MATERIALS
Material Allowables
The structure uses strong composite materials that are chosen to stay reliable in different conditions and over time.
Strategic Operations

SYSTEM INTEGRATION & COLLABORATION

Initialize direct channels for enterprise deployments, open research collaboration, or technical inquiries. Whether you are looking to integrate custom sensing hardware, explore architectural applications, or connect with our engineering roadmap, our ecosystem is open for development.

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