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.

LunaRecycle | NLRS Integrated Mission Profile

LunaRecycle

Integrated Mission Profile // NLS-1

System Readiness

Status Auth 🟡 PRE-FLIGHT CHECKS

Executive Brief

Phase 1

Lunar Surface Recycling:
MSU to Thermal Chamber interface validated.

120W SURVIVAL

15kWh STORAGE

"Operational integrity verified. Solar Particle Event (SPE) protocol initialized in cache. Awaiting SOP clearance."

OTLP Telemetry Node

nls_flux_01 (Radiation Density)

Current Flux

LIVE

Pre-Flight Authorization

SOP Checklists

1 Startup (Cold Start)

Thermal EQ

Battery Temp > 10°C

Dust Purge

EBDM Active 300s

Airlock Integrity

1.0 × 10⁻⁶ atm

2 Batch Logic

NIR Identification

Classify material

Thermal Prep

Ramp to 250°C

Diagnostic Output

Event Log Stream

Risk Architecture

FMEA Severity Index

Execution Traces

Active Span Timings

MSU_Separation 240ms

TPC_PreHeat 1.2s

Airlock_Seal_Chk 85ms

Hardware Health

Consumables & SPE

Airlock Seals 88% OK

MSU Magnets 42% DEPLETED

SPE Threshold Warning

Limit: > 100 MeV flux.
Auto-Action: Initiate Safe State, Retract Secondary Arrays.

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