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03-electric-jet

$4,911,937,500.00

In stock

SKU

2029

Electric Jet: the 30-plate ring in the intake fires pull and push in turn and turns the rotor, the quantum battery charges and feeds it, and air streams out of the back, animated picture

Asset valuation: $5,000,000,000. Price: $5.0 Billion Integration Status: ✅ Quantum Battery Integrated This is the world's first quantum-powered electric jet propulsion system with unlimited range and self-sustaining operation. The system integrates:

For the curious

Imagine a jet that never lands for fuel, because the thing that stores its power also refills it from the light and the fields around it. That is the idea behind the Electric Jet. Its power source is an optical quantum battery: quantum dots in silicon charged by a nano-array of LEDs, with efficiency written at 84 to 98 percent and continuous self-recharge from ambient light and electromagnetic fields. The propulsion is a ring of electromagnetic torque plates, each pulling and pushing on its neighbours around the circle, turning at up to 25,000 rpm. In the thirty-plate configuration it is rated at 4.9 megawatts and 440 kilonewtons of thrust from 860 kilograms, with a Mach 3.19 speed capability, and the same plate scales down to a two-plate drone motor with no redesign.

The archive runs to 341 files: 177 documentation items, 81 source-code modules, CAD drawings and models, and a 64-layer foundry-ready GDSII layout for the battery chip. Five avionics boards, FADEC, inverter, battery management, flight control and main computer, are drawn in KiCad with full bills of materials, written toward DO-178C and DO-254 DAL A certification. Hardware and software trips cover overcurrent, overvoltage, over-temperature, short circuit and ground fault. The maturity level is tape-out, mass-manufacturable.

It is for an aerospace engineering buyer or licensee who wants a propulsion and power system that is already drawn and laid out. The buyer walks away with the full archive; the USPTO applications behind it, the earliest filed in 2023, stay with the inventor, Christopher Gabriel Brown.

Details

Description

Electric Jet — Quantum-Powered Electric Jet Platform (SKU 2029)

Patent Status: Multiple USPTO applications pending. Inventor: Christopher Gabriel Brown .

U.S. Application No. 19/392,226 — “Scalable Electromagnetic Torque Plate System for Jet Propulsion with Optimal Configuration Methodology” — filed November 18, 2025 (Confirmation 5972, Patent Center 73220018)
U.S. Application No. 18/370,908 — “AutoPhi: Quantum Battery Integration & Electromagnetic Propulsion IC” — filed September 21, 2023
U.S. Application No. 19/540,453 — “Integrated Technology Portfolio (umbrella, names Electric Jet Propulsion)” — filed February 13, 2026
U.S. Application No. 19/403,339 — “Optical Quantum Battery System with LED Nano-Charge” — active

Additional priority references: internal patent portfolio numbers #1077, #1078, #1096–1099, #1109–1110. Maturity level 4 — Tape-out / Mass-Manufacturable. License generated 2026-05-02.

Overview

This is the world’s first quantum-powered electric jet propulsion system with unlimited range and self-sustaining operation. The package delivers a complete, production-ready engineering archive — 341 files across 177 documentation items, 81 source-code modules, 28 images, 20 web assets, 12 formal documents, 8 CAD 2D drawings, 3 data files, 3 schematic/firmware sources, 2 archives, 2 CAD 3D models, and 1 GDSII foundry layout. It integrates quantum battery technology (84–98% efficiency, self-recharging) with a scalable electromagnetic torque-plate propulsion system that delivers up to 440 kN of thrust at Mach 3.19 in the optimal 30-plate configuration.

The system scales from a 50 kW drone motor (2 plates) through commercial aircraft (6 plates, 600 kW) to the ultimate 30-plate military configuration (4.9 MW, 440 kN) using the same fundamental physics and design architecture — no redesign required. Five avionics PCB designs (FADEC, inverter, BMS, flight control, main computer) are included as KiCad 10 schematics with full BOMs, targeting DO-178C / DO-254 DAL A certification. A 64-layer foundry-ready GDSII layout for the quantum battery IC is included for tape-out.

Electromagnetic Torque Plate Architecture

Parameter Value

Plate type Electromagnet with soft iron core

Plate dimensions (standard) 150 mm × 150 mm × 20 mm

Core material Silicon steel M19, 0.35 mm laminations, μ r = 4,000

Saturation flux density 1.8 T

Remanence

Magnetic field strength (max) 2.5 T

Coil turns 500 turns per plate

Wire gauge / material AWG 12 copper, Class H insulation (180 °C)

Coil resistance (at 20 °C) 0.08 Ω

Coil inductance 2 mH

Coil fill factor 0.65 (65% copper)

Wire length per coil ~75 m

Wire weight per coil ~1.2 kg

Max current (continuous) 300 A

Max voltage (phase-to-neutral) 400 V

Current density 8 A/mm²

Power rating per plate 50–200 kW (configuration dependent)

Weight per plate ~2.5 kg

Volume per plate 450 cm³

Cooling Liquid-cooled, 4 × 5 mm channels through plate, 2 L/min per plate

Max operating temperature 120 °C

Thermal resistance (junction to coolant) 0.05 °C/W

Mounting 4 × M6, 10 mm from edges

Terminal block 2 × M8 studs, 20 mm spacing

Scalable Configuration Matrix

The system scales from 1 to 50 plates using these scaling laws:

Power: P total = N × P base × (1.0 − (N−1) × 0.002)
Thrust: T = T base × (P / P base ) 0.85
Weight: W = N × W base × 0.95 (N−12) for N > 12
Efficiency: η = 0.92 × (1.0 − (N−1) × 0.002)

Configuration Plates Power Thrust Weight Max RPM Max Torque DC Bus IGBTs Plate Size (mm) Price (hardware)

SMALL (Drone) 2 50 kW 5 kN 25 kg 8,000 600 N·m 400 V 4 100 × 100 × 15 $8,000

MEDIUM (Regional) 4 200 kW 20 kN 75 kg 12,000 1,600 N·m 600 V 8 125 × 125 × 18 $15,000

LARGE (Commercial) 6 600 kW 50 kN 150 kg 15,000 4,000 N·m 800 V 12 150 × 150 × 20 $25,000

XLARGE (Heavy Transport) 10 1,500 kW 125 kN 350 kg 18,000 8,000 N·m 1,200 V 20 200 × 200 × 25 $60,000

MILITARY (Baseline) 12 2,500 kW 200 kN 500 kg 25,000 10,000 N·m 1,500 V 24 250 × 250 × 30 $100,000

ULTIMATE (30-Plate) 30 4,900 kW 440 kN 860 kg 25,000 10,000 N·m 1,500 V 60 250 × 250 × 30 —

30-Plate Ultimate Configuration — Performance

Parameter Value

Total power 4,900 kW (4.9 MW)

Total thrust 440 kN

System weight 860 kg

Thrust-to-weight ratio 3.91 : 1

Maximum RPM 25,000

Maximum torque 10,000 N·m

Efficiency 86%

Exhaust velocity 1,095 m/s

Mach capability 3.19 (hypersonic)

Power per plate 190 kW

Thrust per plate 14.3 kN

Plate dimensions 250 mm × 250 mm × 30 mm

vs. F-35 Lightning II (190 kN) Exceeds by 131%

vs. F-22 Raptor (155 kN) Exceeds by 184%

Power Electronics & Control System

Component Specification

Topology Full-bridge inverter, 3-phase

IGBT module IKW75N120T2 (Infineon) or equiv., 1,200 V / 600 A continuous

Switching frequency 20 kHz

Rise / fall time

Saturation voltage (V ce(sat) ) 2.1 V at 300 A

Gate driver ISO5852S, 5.7 kV isolation, +15 V / −8 V supply

Dead time 2 μs (programmable)

DC link capacitance 10,000 μF, 1,000 V rated, ESR

Current sensor ACS758-400A (Allegro), ±400 A, ±1% accuracy, 120 kHz bandwidth

Voltage sensor Isolated, 0–1,000 V, ±0.5%, 2.5 kV isolation

Microcontroller STM32F407 (ARM Cortex-M4), 32-bit

ADC resolution 16-bit, 1 MSPS

Communication CAN bus 2.0B, 1 Mbps (ISO1050 transceiver)

Control algorithm Field-Oriented Control (FOC) with Space Vector PWM (SVPWM)

Sampling rate 10 kHz (100 μs period)

Current control bandwidth 1 kHz

Speed control bandwidth 100 Hz

Modulation index 0–1.0 (linear), 0–1.15 (overmodulation)

Position/speed sensor Incremental encoder, 4,096 CPR (12-bit), RS422 differential

Operational modes Combat, Afterburner (120% rated), Stealth, Cruise

Compressed Modular Control 3 modules, 500 ms cycle, 166.67 ms per module, sinusoidal on/off, 10% overlap

Protection Systems

Protection Hardware Trip Software Trip Response

Overcurrent 350 A ( 320 A ( Immediate gate shutdown / reduce command

DC link overvoltage 900 V — Braking resistor (10 Ω, 10 kW)

Phase overvoltage 450 V — Inverter shutdown

IGBT over-temperature — Warning 100 °C / Trip 125 °C Power reduction / shutdown

Torque plate over-temp — Warning 100 °C / Trip 120 °C Current reduction / shutdown

Short circuit (desat) V ce > 5 V on-state ( — Immediate gate shutdown

Ground fault 10 mA sensitivity ( — Shutdown & alarm

Quantum Battery Integration

The optical quantum battery system is integrated as the primary self-recharging power source, creating an unlimited-range electric jet platform with zero emissions.

Parameter Value

Battery type Optical Quantum Battery with LED Nano-Array Charging

Efficiency 84–98% (matching AutoPhi Patent 18/370,908)

Self-recharge Continuous from ambient light and EM fields

Energy density 0.1–1 MJ/cm³ (100–1,000× lithium-ion)

Quantum dot array density 10 6 –10 12 dots/cm², silicon, 3–10 nm

LED nano-array density 10 6 –10 12 LEDs/cm², 100–500 nm individual LED size

Magnetic field control 0.1–10 T for quantum coherence

Power output per unit 1 mW to 10,000 mW (scalable to 4,900 kW total)

Capacity range 0.1–5,000 mAh (configurable)

Nominal voltage 3.7 V (programmable 2.5–5.0 V)

Configurations available 10,000+

Manufacturing CMOS-compatible, foundry-ready GDSII

Enclosure 500 mm × 400 mm × 150 mm, Al 6061-T6, IP54, ~20 kg

DC-DC converter 3.7 V → 800 V bus, 90–95% converter efficiency

Overall system efficiency 76–93% (battery × converter)

Voltage regulation ±1% on 800 V bus

Avionics Board Family (5 Boards)

Five aviation-grade PCB designs are included as KiCad 10 schematics with full BOMs and common layout guidance per RTCA DO-160G (operating −55 °C to +85 °C, altitude to 60,000 ft, HIRF Cat R, lightning Cat 3A/L1). Substrate: FR-4 high-Tg (≥ 170 °C).

Board Purpose Form Factor PCB Layers Host Processor DAL (SW/HW) Key Interfaces

EJ-FADEC Full Authority Digital Engine Control (dual-channel per engine) 233 × 160 mm, 3U ATR-half 10-layer 2× TI Hercules TMS570LC4357 (dual lockstep Cortex-R5F) A / A ARINC 429 ×4, CAN-FD ×2, RS-485 ×2, AFDX ×1

EJ-INV EM Propulsion Motor Inverter (2 MW peak, SiC) 500 × 300 mm, 4U cassette 8-layer, 6 oz heavy copper TMS320F28379D DSP + Xilinx Spartan-7 FPGA — / A RS-485 to FADEC; 24× Wolfspeed C3M0016120K SiC MOSFETs; 98.2% efficiency typical

EJ-BMS Quantum Battery Management (4 banks × 8 cells = 32 cells) 300 × 200 mm, 3U ATR-full 10-layer, 4 oz heavy copper — A / A ARINC 429 ×2, CAN-FD ×2; 24-bit per-cell ADC; 4× gated 800 V outputs

EJ-FCS Flight Control / Triple-Redundant Fly-by-Wire 300 × 200 mm, 3U ATR-full 12-layer 3× TMS570LC4357 + FPGA majority-vote arbitrator (2/3 or 3/3) A / A AFDX ×2, ARINC 429 ×8, CAN-FD ×4, discrete IO ×32

EJ-AVI Avionics Main Computer (EFIS + INS/GNSS + comms + Super Dome link) 400 × 250 mm, 6U ATR-full 12-layer 2× NXP LX2160A 16-core Cortex-A72; 32 GB DDR4-3200 ECC; 128 GB eMMC B / B 4× DisplayPort 1.4 to cockpit MFDs (15.4″ 2160×1440), AFDX ×2, ARINC 429 ×16, MIL-STD-1553 ×2, CAN-FD ×4, USB-C ×2; GNSS (u-blox ZED-F9K + Novatel OEM7); INS (Honeywell HG9900); VHF/HF/SATCOM

Deep Physics Modelling

The package includes complete first-principles calculations replacing placeholder values with computed physics:

Domain Formulas / Models

Coil resistance R = ρ(T) × L / A (temperature-dependent resistivity)

Coil inductance L = (μ × N² × A) / l

Magnetic field B = (μ × N × I) / l, with saturation limits

Skin depth δ = √(2ρ / (ωμ))

Proximity effect Multi-layer winding loss model

Copper losses P copper = I² × R

Hysteresis losses P hyst = k h × f β × B α × V (Steinmetz, α = 1.6)

Eddy current losses P eddy = (π² × f² × B² × t² × V) / (6 × ρ)

IGBT switching losses P sw = (E on + E off ) × f sw

IGBT conduction losses P cond = V ce(sat) × I × D

3D thermal conduction R θ = t / (k × A)

Convective heat transfer h = (Nu × k) / D (Nusselt correlations)

Transient thermal response T(t) = T amb + (T ss − T amb ) × (1 − e −t/τ )

Thrust scaling T = T base × (P / P base ) 0.85

Efficiency (overall) η = P out / (P out + P losses )

Throttle mapping P setpoint = (throttle% / 100)² × P max (configurable linear/squared)

Thermal Management

Parameter Value

Coolant 50/50 water-glycol, 5 L system volume

Flow rate (optimised) 70 L/min (system), 2 L/min per plate

Operating temperature range 30–50 °C coolant

Total system heat dissipation 77 kW (33.8 kW IGBTs + 43.2 kW plates)

Radiator 600 × 400 × 50 mm × 2 units, 20 fins per 10 mm, 2× 120 mm fans at 200 CFM each

Pump Centrifugal, 70 L/min at 3 bar, 200 W, 12 V DC

Freeze point −35 °C

Steady-state IGBT junction 125 °C (max)

Steady-state plate core 80 °C

Time to steady state ~1,250 s (5τ, τ = 250 s)

EMI / EMC Compliance

Standard Scope

CISPR 11 Industrial / scientific / medical equipment

CISPR 22 Information technology equipment

IEC 61000-4 Immunity (ESD ±8 kV contact / ±15 kV air, radiated 10 V/m, conducted 10 V, surge ±2–4 kV)

MIL-STD-461 Military equipment

FCC Part 15 US commercial

DO-160G Aviation environmental (temperature, altitude, vibration, HIRF, lightning)

Mitigation includes input pi-filter (L-C-L, > 40 dB at 20 kHz), output common-mode choke (5 mH, 300 A/phase), aluminum 6061 enclosure with EMI gaskets (> 60 dB shielding 1 MHz–1 GHz), star grounding, via fencing, and TVS / varistor protection on all I/O. Post-mitigation margin: +15 dB at 100 kHz, +27 dB at 100 MHz.

PCB & Gerber Specifications

Parameter Value

Board size 200 × 150 mm

Layer count 6 (signal + ground + power + high-power + ground + signal)

Material FR-4, Tg 170 °C

Total thickness 1.5 mm

Copper weight 2 oz (70 μm) outer, 1 oz (35 μm) inner

Surface finish ENIG

Gerber format RS-274X (Extended Gerber), mm, 3.4 coordinate

Gerber file count 15 files (top/bottom copper, solder mask, silkscreen, paste, 4 inner layers, drill PTH/NC, outline)

Quality standard IPC-A-600 Class 2, IPC-A-610 Class 2

Panelisation 400 × 300 mm, 4 boards (2×2), 5 mm spacing

Test points 30 (DC link, phase currents, gate signals, temperatures, control signals)

Manufacturing & Assembly

The package includes step-by-step manufacturing procedures for torque plate lamination stacking, coil winding (500 turns, AWG 12, Class H insulation), PCB assembly (SMD pick-and-place, through-hole, reflow + wave solder, X-ray inspection), IGBT mounting with thermal paste, cooling system plumbing, and full system integration. Assembly torque: 8–12 N·m for torque plate mounts, 5–8 N·m for DC link / inverter, medium-strength threadlock (Loctite 243 or equivalent). Crimp reference covers 2/0 AWG to 22 AWG with minimum pull forces.

3D Print & CAD Package

Deliverable Format Purpose

Parametric 3D model OpenSCAD (.scad) Editable assembly — exploded or assembled view; export single part or full assembly as STL

2D dimensioned views SVG, DXF (via export_electric_jet_dxf.py) AutoCAD / LibreCAD

STEP 3D model ISO 10303-21 (.stp) SolidWorks / CATIA / Inventor import

Wiring diagram SVG Harness build reference

Wire list Markdown table W01–W09 wire IDs, gauges, routing

BOM — 8 find-number assemblies: EJ-03-CORE-001 (Al 6061 frame), EJ-03-TP-001 (torque plate ×6), EJ-03-DC-001 (DC link housing, PEEK), EJ-03-PWR-001 (800 V bus enclosure), EJ-03-INV-001 (inverter module ×2), EJ-03-QB-001 (quantum battery housing), EJ-03-COOL-001 (cooling manifold), EJ-03-SENS-001 (sensor block), plus EJ-03-HARN-001 harness. Tolerancing: ±0.5 mm general, ±0.05 mm critical. Surface finish: Ra 3.2 (6.3 non-critical). Third-angle projection, ASME Y14.5.

Foundry Handoff & GDSII

Item Detail

GDSII file GEN6_QUANTUM_01141_COMPLETE_64LAYER.gds

Layer count 64 layers

Design Quantum battery IC with LED nano-charging arrays

Status Ready for foundry submission

Standalone generator GDSII_GENERATOR_STANDALONE_CD.zip

Software Suite

Module Language Purpose

main.py Python / Flask Production-ready web server (port 8080)

motor_control.py Python Hardware interface layer

simulation.py Python Real-time propulsion simulator

api.py Python REST API (GET /api/status, POST /api/control, GET /api/configurations)

scaling_calculator.py Python Calculate any arbitrary plate configuration

test_suite.py Python Validation & acceptance tests

throttle_map.py Python Throttle-to-power mapping (linear / squared); PWM duty to throttle with deadband

dashboard.html HTML/JS Modern real-time web dashboard

motor_controller.ino Arduino C++ Embedded controller — PID + compressed modular control, safety monitoring

military_motor_controller.ino Arduino C++ Military-grade embedded controller

commercial_motor_controller.ino Arduino C++ Commercial embedded controller

electromagnetic_jet_motor.py Python Core motor physics model

military_grade_motor.py Python Military configuration model

commercial_jet_motor.py Python Commercial configuration model

control_interface.py Python Control system interface

detailed_electromagnetic_design.py Python Detailed EM design generator

scalable_designs.py Python Multi-config design generator

blueprint_generator.py Python Automated blueprint generation

physics_calculator.py Python Electromagnetic physics calculations

advanced_physics_calculator.py Python Skin depth, proximity, comprehensive loss models

enhanced_motor_calculations.py Python Enhanced motor performance modelling

complete_plate_scaling.py Python Full 1–50 plate scaling analysis

ultimate_plate_analysis.py Python 30-plate optimal configuration analysis

generate_all_outputs.py Python Generate all engineering output files

output_file_generator.py Python Parametric output file generation

export_electric_jet_dxf.py Python DXF export for AutoCAD

gen_schematic.py Python KiCad schematic generator for avionics boards

electric_jet_assembly.scad OpenSCAD Parametric 3D model (exploded/assembled, single-part export)

Front-end JavaScript modules (7 files): dashboard.js, drone-fleet.js, energy.js, flight-management.js, main.js, navigation.js, propulsion.js. Stylesheets: main.css.

Quantum battery integration scripts (40+ Python modules) cover battery array calculation, configuration generation (100+ configs, extended configs), rapid cycling analysis, CMOS performance optimisation, manufacturing cost calculation, foundry handoff generation, efficiency analysis, and comprehensive revaluation.

Cost Analysis (LARGE / 600 kW Configuration)

Category Cost (per unit, 10-unit run)

Power electronics $2,880

Control electronics $80

Torque plates (×6) $1,620

Mechanical components $1,560

PCB fabrication & assembly $900

EMC components $800

Total components $7,840

Production unit cost (at 100 units) ~$23,383

10-year life-cycle cost $1,275,000 (vs. $9,000,000 conventional jet — 86% saving)

Payback period 15 days

Formal Engineering Drawings (CAD 2D)

Drawing No. Title Format

EM-JET-001 Main Assembly .dwg, .stp

AS-001 Assembly Sequence .dwg

TP-001 Torque Plate — Standard .dwg

PE-001 Power Electronics Board .dwg

DWG-001 Assembly Dimensioned (principal dims) .svg

QB-001 Quantum Battery Enclosure (in docs)

QB-002 Quantum Battery Array Module (in docs)

QB-003 DC-DC Converter Module (in docs)

Patent illustration SVGs: 4 formal patent figures (PATENT_ILLUSTRATION_01 through 04) plus 8 technical figures (FIG1 System Architecture through FIG8 Deep Physics Modeling).

Bill of Materials — Key Components

Part No. Description Qty Unit Price Supplier

TP-001 Torque plate (Si steel M19 + Cu coil, wound) 6 $1,200 Internal

IGBT-001 IGBT IKW75N120T2 (1,200 V / 600 A) 12 $150 Infineon

GD-001 Gate driver ISO5852S (5.7 kV isolation) 6 $25 TI

CAP-001 DC link capacitor 10,000 μF / 1,000 V 10 $80 Panasonic

CS-001 Current sensor ACS758-400A 6 $15 Allegro

MCU-001 STM32F407 (ARM Cortex-M4) 1 $15 ST

ENC-001 Encoder 4,096 CPR optical incremental 1 $200 Avago

ENCL-001 Enclosure Al 6061-T6 (400×300×200 mm) 1 $500 Internal

COOL-001 Cooling system (pump + radiator + hoses) 1 $500 Internal

PCB-001 6-layer PCB fabrication (200×150 mm) 1 $500 PCB house

Total BOM (LARGE config) $14,371

Test & Acceptance

Step Test Pass Criteria

1 Insulation 800 V to frame ≥ 1 MΩ at 500 V DC

2 Continuity W01–W09 per Wire_List; no shorts

3 Power-up 800 V bus 800 V ±5%; throttle 0% → no drive

4 Throttle ramp 0% → 20% → 50% → 100%; bus current follows; no fault

5 Thrust (test stand) Thrust cell within 15% of predicted for given power

6 E-stop / Enable Enable low or heartbeat off; drive off

Documented requirements: 10 formal requirement IDs (REQ-EJ-03-001 through REQ-EJ-03-010) with full traceability matrix linking each requirement to its source specification and test procedure.

What Is in the Package

341 files total (166 .md, 74 .py, 26 .svg, 19 .html, 11 .txt, 11 .pdf, 8 .dwg, 7 .js, 3 .ino, 2 .zip, 2 .json, 2 .png, 1 .scad, 1 .docx, 1 .stp, 1 .gds, 1 .css, 1 .csv, 1 .cff, 1 LICENSE, 1 .code-workspace)
blueprints/ — 85+ entries: torque plate designs, power electronics, electromagnetic design (JSON + Python), scalable configuration generator, 12 SVG technical illustrations, 4 patent illustration SVGs, 8 formal figure SVGs, 7 JavaScript front-end modules, web dashboard, CSS stylesheet, DWG drawings (EM-JET-001, AS-001, TP-001, PE-001), patent application documents (USPTO format .txt + .md), Aeronautical Blueprint Standards, Project Status Report, sales pitch materials, CD-ROM navigation page, VS Code workspace
blueprints/engineering/ — Detailed Design Specifications, 3D Mechanical Drawings, Cost Analysis, EMI/EMC Considerations, Manufacturing Procedures, PCB Layout & Gerber Specifications, Thermal Analysis, Configuration Matrix, Calculated Values Summary, Deep Physics Integration, Scaling Summary, Plate Scaling Rationale, Ultimate Plate Answer, Multi-Conductor Plate Analysis, Placeholder Replacement Logs, Output Files Guide; 9+ Python calculators (physics, advanced physics, enhanced motor, plate scaling, output generation); STEP 3D model; CSV BOM; Drawing Index; Patent Illustrations README
blueprints/engineering/embedded_control/ — 3 Arduino .ino firmware files (motor_controller, military_motor_controller, commercial_motor_controller)
blueprints/PRODUCT_PACKAGE/ — Complete sellable product: main.py, motor_control.py, simulation.py, api.py, scaling_calculator.py, test_suite.py; dashboard.html template; run.bat & run.sh launch scripts; requirements.txt; README, INSTALL, SELLING_GUIDE, SMALL_CONFIG_SPECS, VALIDATION_TEST_PLAN, PRODUCT_MANIFEST documentation
blueprints/quantum-battery-integration/ — 80+ files: battery array calculator, configuration generators (100+ configs, extended, 5,000-unit), rapid cycling analysis, CMOS performance optimisation, manufacturing cost calculator, foundry handoff creator, efficiency analysis and validation, entity valuation, Buford Dam equivalence comparison, hybrid dam system analysis, household and urban battery integration, AR coating integration, LED power recycling synthesis and verification, three battery systems analysis, comprehensive revaluation scripts, Magento gallery generators, Blu-ray menu organiser, SVG gallery tools; plus 50+ markdown analysis and summary documents
hardware/ — 5 avionics board packages (EJ_FADEC, EJ_INV, EJ_BMS, EJ_FCS, EJ_AVI), each with SPEC.md, BOM.csv, and KiCad 10 schematic (.kicad_sch); common layout guidance (AVIONICS_COMMON_LAYOUT.md); schematic generator script (gen_schematic.py)
drawings/ — DWG-001_Assembly_Dimensioned.svg, Wiring_Diagram.svg, Wire_List.md, Inventor Drawing Package, Manufacturing Checklist, Part Drawing Index, README
3d_print/ — electric_jet_assembly.scad (OpenSCAD parametric 3D model, exploded/assembled views, single-part STL export), README
specs/ — 10 documents: REAL_SPECS (production-ready electrical/propulsion/throttle/connector/thermal/test), ASSEMBLY_DETAIL, CONNECTOR_AND_THROTTLE_SPEC_DETAILED, DETAILED_TEST_PROCEDURE, DOCUMENT_CHANGE_LOG, MODERN_DESIGN_ELEMENTS, PERFECT_MODEL_SPEC, QUALIFICATION_SUMMARY, REQUIREMENTS_LIST, TRACEABILITY_MATRIX
software/ — SOFTWARE_SPEC_MAPPING.md, throttle_map.py
scripts/ — export_electric_jet_dxf.py (DXF export for AutoCAD)
handoffs/ — Foundry handoff README, GDSII file (GEN6_QUANTUM_01141_COMPLETE_64LAYER.gds, 64-layer quantum battery IC), images.zip
patent-receipts/ — USPTO Patent Application (full text), Abstract Page, Fee Transmittal Form, Oath or Declaration, 4 Essential Forms (fee transmittal, PTO/AIA/34, PTO/SB/01, PTO/SB/16 — filled PDFs)
sales-pitches/ — 26 files: complete package sale, individual sales guide, investor pitch deck, licensing proposal, outreach emails, sales package, sales summary, email campaigns with NDA, master price sheet, agreement tracker, communication policy, product card, store product description, vault delivery instructions, 10 Proof of Function HTML demos, Proof of Function Listings
product-images/ — Product image (695825296495-2.png)
Root-level files: README.md, README_SPECS_AND_SOFTWARE.md, PLAYBOOK.md, MANIFEST.json, LICENSE (proprietary), CITATION.cff, CHANGELOG.md, CONTACT_INFO.txt, HANDOFF_BLURB.md, RENDER_SPECIFICATION.md, WEB_DESCRIPTION.html, GDSII_GENERATOR_STANDALONE_CD.zip

How this is delivered

This package ships on a single Blu-ray disc, posted to the delivery address on your order. The archive on the disc is AES-256 encrypted; the passphrase is sent separately, by email, once the disc is despatched — so the disc alone is of no use to anyone who intercepts it.

Discs are despatched by tracked, signed-for post. Allow 5 business days for mastering and verification before despatch.

Photo

Bench test rig in an aluminium frame with motor discs, a 'DC LINK' box and a 'QUANTUM BATTERY' box

Footnotes

Product number 8448.
Family: electromagnetic propulsion.
Purchase: When you buy, you buy the use of that blueprint only.

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