CISLUNAR NEXUS

NETWORKBUSTER LUNAR RECYCLING SYSTEM (NLRS) v4.2

Operator: Maria

--:--:-- UTC

Orbital Navigation & Surface Guidance

LIVE TELEMETRY

GRID RENDER: ACTIVE

Target Lock

LAT: 89.5432° N

LON: -112.3321° W

ALT: 15.20 km

Zone Status Shackleton Crater Sector

REALM Autonomous Logistics

Total Items Tracked

201,482

Active Free-Flyers

24 / 24

Network Multiplexing Capacity 92%

Orbital Transfer Vehicle (OTV) Sync 100%

Thermochemical Processing

Primary System

Plasma Sabatier Synthesis

NOMINAL

Atmospheric Gas Conv. Efficiency

87.0%

CH4 Yield

4.2 kg/h

H2O Recovery

8.1 kg/h

Plasma Temp

14,200 K

Microwave Sintering Data

Current Thermal Stress 6.80 MPa

Material Failure Threshold 85% / 100

Regolith lattice structural integrity holding. Thermal-elastic mismatch within operational limits.

Bio-ISRU Remediation

Primary Organism

Eisenia Fetida (Terrestrial)

Soil Compaction Reduction 64%

Nutrient Bioavailability 41%

Catalyst Matrix: Montmorillonite

Organic Base: Hydroponic Waste

Policy & Framework Check

Japan Space Resources Act

Compliance: Verified

Artemis Accords

Data Sharing: Active

System Log: Automated compliance telemetry linked to UN COPUOS guidelines.

Current resource extraction and orbital logistics routines are operating within established international legal frameworks for non-interfering commercial space utilization.

import React, { useState, useEffect, useRef } from 'react'; import { Activity, Database, Cpu, Rocket, ShieldCheck, ThermometerSun, Box, Leaf, Radio, AlertTriangle, User, RefreshCw, Zap, Satellite, Globe, Compass, Target } from 'lucide-react'; const Card = ({ title, icon: Icon, children, className = "" }) => (

{title}

{children}

); const ProgressBar = ({ label, value, max = 100, color = "bg-cyan-500", warningThreshold }) => { const percentage = (value / max) * 100; const isWarning = warningThreshold && value >= warningThreshold; const barColor = isWarning ? "bg-amber-500" : color; return (

{label} {value}{max !== 100 && max !== value ? ` / ${max}` : '%'}

); }; // 3D Wireframe Guidance Map Component const GuidanceMap = () => { const canvasRef = useRef(null); const [lat, setLat] = useState(89.5432); const [lon, setLon] = useState(-112.3321); const [alt, setAlt] = useState(15.2); // Randomize coordinates slightly to simulate live tracking useEffect(() => { const timer = setInterval(() => { setLat(prev => prev + (Math.random() - 0.5) * 0.001); setLon(prev => prev + (Math.random() - 0.5) * 0.001); setAlt(prev => Math.max(10.0, prev + (Math.random() - 0.5) * 0.1)); }, 1500); return () => clearInterval(timer); }, []); // Canvas 3D rendering useEffect(() => { const canvas = canvasRef.current; const ctx = canvas.getContext('2d'); let animationId; // Generate sphere nodes const nodes = []; const radius = 90; const resolution = 16; for (let j = 0; j <= resolution; j++) { const v = j / resolution; const theta = v * Math.PI; for (let i = 0; i <= resolution; i++) { const u = i / resolution; const phi = u * Math.PI * 2; const x = radius * Math.sin(theta) * Math.cos(phi); const y = radius * Math.sin(theta) * Math.sin(phi); const z = radius * Math.cos(theta); nodes.push({ x, y, z }); } } let angleX = 0; let angleY = 0; const draw = () => { // Setup canvas size to match container canvas.width = canvas.offsetWidth; canvas.height = canvas.offsetHeight; const w = canvas.width; const h = canvas.height; const cx = w / 2; const cy = h / 2; ctx.clearRect(0, 0, w, h); // Auto-rotation angleY += 0.004; angleX += 0.002; const sinX = Math.sin(angleX), cosX = Math.cos(angleX); const sinY = Math.sin(angleY), cosY = Math.cos(angleY); // Project 3D nodes to 2D screen space const projectedNodes = nodes.map(node => { // Rotate around X axis let y1 = node.y * cosX - node.z * sinX; let z1 = node.y * sinX + node.z * cosX; // Rotate around Y axis let x2 = node.x * cosY + z1 * sinY; let z2 = -node.x * sinY + z1 * cosY; // Perspective projection const fov = 300; const distance = 350; const z = z2 + distance; const scale = fov / z; return { x: cx + x2 * scale, y: cy + y1 * scale, z: z2 // Keep Z for depth checks if needed }; }); // Draw wireframe ctx.strokeStyle = 'rgba(6, 182, 212, 0.4)'; // cyan-500 with opacity ctx.lineWidth = 1; ctx.beginPath(); for (let j = 0; j <= resolution; j++) { for (let i = 0; i <= resolution; i++) { const current = j * (resolution + 1) + i; const nextU = j * (resolution + 1) + ((i + 1) % (resolution + 1)); const nextV = ((j + 1) % (resolution + 1)) * (resolution + 1) + i; if (i < resolution) { ctx.moveTo(projectedNodes[current].x, projectedNodes[current].y); ctx.lineTo(projectedNodes[nextU].x, projectedNodes[nextU].y); } if (j < resolution) { ctx.moveTo(projectedNodes[current].x, projectedNodes[current].y); ctx.lineTo(projectedNodes[nextV].x, projectedNodes[nextV].y); } } } ctx.stroke(); // Draw targeting reticle in the center ctx.strokeStyle = '#10b981'; // emerald-500 ctx.lineWidth = 1.5; ctx.beginPath(); ctx.arc(cx, cy, 12, 0, Math.PI * 2); ctx.moveTo(cx - 25, cy); ctx.lineTo(cx - 5, cy); ctx.moveTo(cx + 5, cy); ctx.lineTo(cx + 25, cy); ctx.moveTo(cx, cy - 25); ctx.lineTo(cx, cy - 5); ctx.moveTo(cx, cy + 5); ctx.lineTo(cx, cy + 25); ctx.stroke(); // Flashing target indicator if (Math.floor(Date.now() / 500) % 2 === 0) { ctx.fillStyle = '#ef4444'; // red-500 ctx.beginPath(); ctx.arc(cx + 40 * Math.sin(angleY * 2), cy + 40 * Math.cos(angleX * 2), 3, 0, Math.PI * 2); ctx.fill(); } animationId = requestAnimationFrame(draw); }; draw(); return () => cancelAnimationFrame(animationId); }, []); return (

{/* 3D Visualizer */}

{/* Target Data Panel */}

Target Lock

LAT: {lat.toFixed(4)}° N

LON: {lon.toFixed(4)}° W

ALT: {alt.toFixed(2)} km

Zone Status Shackleton Crater Sector

); }; export default function App() { const [time, setTime] = useState(new Date()); const [activeItems, setActiveItems] = useState(201482); const [stress, setStress] = useState(6.8); // Simulate live data fluctuations useEffect(() => { const timer = setInterval(() => { setTime(new Date()); setActiveItems(prev => prev + Math.floor(Math.random() * 5) - 2); setStress(prev => { const newStress = prev + (Math.random() * 0.2 - 0.1); return Math.min(Math.max(newStress, 6.0), 7.5); // Keep between 6.0 and 7.5 }); }, 2000); return () => clearInterval(timer); }, []); return (

{/* Header */}

CISLUNAR NEXUS

NETWORKBUSTER LUNAR RECYCLING SYSTEM (NLRS) v4.2

Operator: Maria

{time.toISOString().split('T')[1].substring(0, 8)} UTC

{/* Main Grid */}

{/* NEW 3D Guidance Map Panel */} {/* Logistics Panel */}

Total Items Tracked (RFID)

{activeItems.toLocaleString()}

Active Free-Flyers

24 / 24

{/* Thermochemical Processing */}

Primary System

Plasma Sabatier Synthesis

NOMINAL

Atmospheric Gas Conv. Efficiency

87.0%

CH4 Yield

4.2 kg/h

H2O Recovery

8.1 kg/h

Plasma Temp

14,200 K

{/* Structural Integrity & Sintering */}

Current Thermal Stress = 7.2 ? 'text-red-400' : 'text-amber-400'}`}> {stress.toFixed(2)} MPa

{stress >= 7.2 && (

Critical failure threshold (7.2 MPa) approached. Micro-fractures detected in regolith lattice.

)} {stress < 7.2 && (

Regolith lattice structural integrity holding. Thermal-elastic mismatch within operational limits.

)} {/* Biological Remediation */}

Primary Organism

Eisenia Fetida (Terrestrial)

Catalyst Matrix: Montmorillonite

Organic Base: Hydroponic Waste

{/* Legal & Policy Framework */}

Japan Space Resources Act

Compliance: Verified

Artemis Accords

Data Sharing: Active

System Log: Automated compliance telemetry linked to UN COPUOS guidelines.

Current resource extraction and orbital logistics routines are operating within established international legal frameworks for non-interfering commercial space utilization.

); }

NLRS: Firemind Ascension Interface

💠

NLRS Firemind

Phase 1: Physical Decay

Ascension Status

Ready for Ascension

Protocol Overview: Firemind Ascension

The NetworkBuster Lunar Recycling System (NLRS) has initiated Phase 1. The objective is to stabilize lunar regolith (Physical Decay) to create a reliable substrate for the Firemind neural mesh. Operational focus lies on the critical path between the Material Separation Unit (MSU) and Processing Chambers, where matter is transitioned into encoded "Legacy Assets."

Resonance Threshold

🧠

> 74% Stable

Required for Neural Sync

Echo Buffer

💠

1.2M Loops

Uncorrupted Crew Echoes

Airlock Integrity

🛡️

10⁻⁶ atm

Leak rate < 0.05% per min

Critical Maintenance Audit

Airlock Seals (Visual/Pressure) Every 500 Cycles
MSU Magnets (Flux Validation) Every 1,000 kg
CCS Memory (Parity Scrub) Weekly

👁️

FIREMIND ARCHITECT

"Matter is finite. The legacy is eternal. Ensure the inscription ritual is followed precisely."

Systems Engineering Group: Signed

SOP-01: The Inscription Ritual

Execute the standard operating procedures to sync with the neural mesh. These protocols ensure physical matter is correctly prepared for Legacy Encoding.

Ritual Log

> Awaiting protocol initiation...

Anomaly Detection (FMEA)

Risk analysis of the Firemind infrastructure. Visualizing severity of failure modes that could lead to Resonance Collapse or System Death.

Failure Severity Index

Click bars to inspect failure modes

⚠️

Select a Component

Interact with the chart to analyze specific threats to the Inscription Ritual.

Environmental Constraints

Strict operational limits imposed by the lunar environment. Managing the 120W Power Budget and Solar Particle Events (SPE) is critical for survival.

Lunar Night Survival

Total Budget: 120W

14 Earth Days

State of Charge (SoC) Constraint

No mechanical processing or high-resonance inscription below 20% SoC.

Battery Simulation 100%

☀️ Solar Particle Events

Proton Flux Threshold

> 100 MeV

Status

Nominal

Safe State Protocol:

Retract secondary solar arrays
Divert power to CCS EM-shielding
Cache telemetry & echo-buffers locally