PROJECT MARK II

SYSTEMS INTEGRATION ARCHITECTURE

Hybrid Flight, Advanced Telemetry & Adaptive Energy Matrix

FROM STATIC COSPLAY TO FUNCTIONAL FLIGHT SYSTEM

Open-Source Development Proposal | MIT / GNU GPLv3 / Open Hardware

THE EVOLUTION: MARK I → MARK II

MARK I

Static Foundation

Cosmetic Sensors

Basic LED reactor prop

Basic Actuators

Helmet kinematics only

Local Operation

No autonomous control

MARK II

Flight-Capable System

LIFT

VTOL without fossil fuels

POWER

Autonomous energy supply

CONTROL

FCS stabilization system

PROPOSED SOLUTION

EDF Propulsion

+

Vacuum-Compression

+

4-Cell Battery

PHYSICAL TOPOLOGY: ANATOMICAL ARCHITECTURE

DORSAL AXIS

Primary Thrusters M1/M2

75% Lift Force

VTOL Capability

Scapular Mounts

COSTAL AXIS

Secondary Thrusters M3/M4

Stabilization System

Thrust Vectoring

Gimbaled Mounts

ENERGY STORAGE

Battery Configuration

4x Li-Po Batteries

Saddlebag Layout

CoG Optimization

CENTRAL PROCESSING

Flight Computer Core

FCS Mainboard

PMIC Integration

Frontal Pectoral Mount

EDF PROPULSION UNIT

Electric Ducted Fan Technology

HYBRID FLIGHT DYNAMICS: PROPULSION MECHANICS

TWO-STAGE PROPULSION SYSTEM

STAGE 1

VTOL Liftoff

• Maximum Torque

• Vacuum-Assisted Lift

• Ignition Phase

STAGE 2

Aerospace Cruise

• Ram-Air Activation

• Reduced Electrical Load

• Passive Thrust

VACUUM PHYSICS MODEL

50%

Electrical Motor

+

50%

Atmospheric Vacuum

=

50%

Battery Drain Reduction

THRUST VECTORING

Gimbaled M3/M4 Motors

Pitch Control

Roll Adjustment

Yaw Stabilization

THRUST-TO-WEIGHT RATIO

VTOL Requirement: > 1:1

Vacuum contribution reduces sustained power draw by ~50% during cruise

OMNIDIRECTIONAL ENERGY MATRIX: PERPETUAL POWER

MULTI-SOURCE HARVESTING

PIEZOELECTRIC KINETIC

Boot sensors convert movement to charge • Japanese pedestrian technology

PHOTOVOLTAIC LAYER

Flexible solar arrays in armor • Daytime harvesting

ATMOSPHERIC TESLA TOWER

RF energy & static potential capture • Trickle-charge standby systems

UNIVERSAL COMPATIBILITY

Qi Wireless Induction

Device-to-Suit Transfer

Multi-Chemistry Adapter

LiPo • Li-Ion • Alkaline

REDUNDANT BMS

Battery Cells:

4x

Auto-Switch Threshold:

15%

J.A.R.V.I.S. CORE: THE BRAIN

SOFTWARE ARCHITECTURE

BLE SENSOR NETWORK

• Wireless Telemetry

• UUID Pairing

• Encrypted Transmission

• Reduced Wiring Weight

FAILSAFE PROTOCOLS

• Limp Mode

• Auto-Land Descent

• PID Control System

• Automotive Diagnostics

HUD & AR INTEGRATION

• Artificial Horizon

• Thermal Map (ATMS)

• Battery Status

• Altitude/Speed

• Collision Warnings

• System Health

OPERATION MODE

10ms

Scan Loop Rate

KEY PROTOCOLS

Protocol Hot-Swap

Protocol Fallback

Auto-Land Sequence

SYSTEM ARCHITECTURE OVERVIEW

FCS

Flight Control System

Central OS

BLE

Bluetooth Low Energy

Sensor Network

EDF

Electric Ducted Fan

Propulsion

BMS

Battery Management

Safety System

ATMS

Active Thermal Mgmt

Cooling System

PMIC

Power Management IC

Voltage Stabilizer

HUD

Heads-Up Display

Data Projection

MEMS

Micro-Electro-Mechanical

Gyroscopic Sensors

THRUST-TO-WEIGHT

> 1:1

VTOL Requirement

BATTERY CONFIG

4x Li-Po

Redundant System

EFFICIENCY GAIN

50%

Vacuum Contribution

OPEN-SOURCE DEVELOPMENT INITIATIVE

100% BASED ON EXISTING TECHNOLOGIES

Individual components exist commercially.
Innovation lies in the integration of these systems.

LICENSE

MIT / GNU GPLv3

Open Hardware

DOCUMENT

EXO-ATMOS-001

Version 1.0.0

INSPIRATIONS

Nikola Tesla

Iron Man Universe

JOIN THE DEVELOPMENT COMMUNITY

Open-Source Development Proposal • Platform: GitHub / Notion