MISSION ARCHIVES

Mission plans, engineering specs, research papers, and Starship data

════════════════════════════════════════════════════════════════════════

C:\MOON\ARCHIVES> dir /missions /all

MISSION PLANS: 4 documents

ENGINEERING SPECS: 5 documents

RESEARCH PAPERS: 4 documents

TOTAL ARCHIVE SIZE: 22 classified documents

────────────────────────────────────────────────────────────────────────

// SELECT_CATEGORY

────────────────────────────────────────────────────────────────────────

// DOCUMENT_INDEX [22 files]

Artemis V - Lunar South Pole Landing Plan2026-Q3

Full mission architecture for crewed Starship HLS landing at Shackleton Crater rim

Source: NASA / SpaceX[MISSION-PLANS]
Permanent Outpost Phase 1 - Foundation Blueprint2027-Q1

Initial habitat deployment, power grid installation, and ISRU proof-of-concept schedule

Source: SpaceX Lunar Division[MISSION-PLANS]
Cargo Pre-Deployment Manifest - Missions C1 through C62026-Q1

Six uncrewed Starship cargo deliveries: rovers, regolith processors, solar arrays, supplies

Source: SpaceX Mission Planning[MISSION-PLANS]
Crew Rotation Protocol - 180-Day Tours2028-Q2

Crew selection, training pipeline, rotation schedule, and emergency evacuation procedures

Source: NASA Astronaut Office[MISSION-PLANS]
Starship HLS Block 2 - Technical Specifications2025-11-15

Revised lunar lander variant with extended cargo bay and improved landing gear for regolith

Source: SpaceX Engineering[ENGINEERING]
Raptor 3 Engine - Lunar Descent Profile Analysis2025-08-20

Throttle curves, fuel margins, and abort mode capabilities for powered lunar descent

Source: SpaceX Propulsion[ENGINEERING]
Orbital Refueling Architecture - LEO Depot Design2025-06-10

Tanker flight cadence, propellant transfer mechanism, and boiloff mitigation strategies

Source: SpaceX Engineering[ENGINEERING]
Lunar Surface EVA Suit - Mark IV Design Review2026-01-12

Next-gen pressure suit rated for 8-hour EVAs in lunar dust environment

Source: Axiom Space / NASA[ENGINEERING]
Communication Relay Constellation - Lunar South Pole2025-09-30

Frozen orbit relay satellites for continuous Earth-Moon-base connectivity

Source: NASA SCaN / SpaceX[ENGINEERING]
Lunar Regolith Toxicology - Inhalation Risk Assessment2024-07-15

Characterization of sub-micron lunar dust particles and respiratory damage models

Source: NASA JSC / ESA[RESEARCH]
Galactic Cosmic Ray Shielding - Regolith Berm Effectiveness2024-11-22

Monte Carlo simulations of radiation dose reduction using 2m regolith overburden

Source: NASA SRAG[RESEARCH]
Water Ice Concentration Map - Shackleton Crater PSRs2025-03-08

LCROSS and orbital radar data synthesis: estimated 5-10% ice by mass in upper 2m

Source: NASA GSFC / JAXA[RESEARCH]
Closed-Loop Life Support - 365-Day Trial Results2025-05-20

ISS-based ECLSS expansion test: 94% water recovery, 78% oxygen regeneration achieved

Source: NASA MSFC[RESEARCH]
Starship IFT-7 Post-Flight Analysis2025-04-12

Full orbital insertion, payload deployment, and controlled ocean landing achieved

Source: SpaceX[STARSHIP]
Starship Tanker Variant - Rapid Turnaround Data2025-10-01

14-day pad turnaround demonstrated; target 7-day cadence for depot filling campaign

Source: SpaceX Boca Chica[STARSHIP]
Starship Heat Shield V2 - Reentry Performance2025-07-18

Upgraded tile system survives 10+ reentries; critical for tanker economics

Source: SpaceX Thermal[STARSHIP]
Inflatable Habitat Module - Pressure Test Report2025-12-05

Bigelow-derived expandable module: 300 cubic meters habitable volume per unit

Source: SpaceX / Sierra Space[HABITAT]
Sintered Regolith Construction - Robotic 3D Printing2025-08-14

Microwave sintering of lunar soil into structural bricks at 1.5 bricks per hour

Source: ICON / NASA[HABITAT]
Radiation Storm Shelter - Emergency Protocol Design2026-02-01

Central water-wall shelter rated for 72-hour SPE protection for 12 crew members

Source: SpaceX Lunar Division[HABITAT]
ISRU Pilot Plant - Water Extraction from Regolith2025-11-28

Thermal extraction system producing 500 kg water per month from icy regolith feedstock

Source: NASA KSC / SpaceX[ISRU]
Lunar Oxygen Production - Electrolysis System Design2025-09-15

Solid oxide electrolysis splitting water ice into O2 and H2 for propellant and breathing

Source: NASA GRC[ISRU]
Propellant Depot - Lunar Surface Storage Architecture2026-01-20

Cryogenic LOX/LH2 storage in permanently shadowed crater alcove; zero boiloff design

Source: SpaceX / ULA[ISRU]
────────────────────────────────────────────────────────────────────────

// ARCHIVE_INFO.TXT

This archive contains key mission documents for the lunar settlement program led by SpaceX in partnership with NASA and international space agencies. Documents include mission architectures, engineering specifications, habitat designs, ISRU studies, and Starship flight data.

All documents are compiled from public NASA reports, SpaceX mission updates, and peer-reviewed research. Some specifications may be preliminary pending final design reviews.

────────────────────────────────────────────────────────────────────────

// KEY_METRICS.TXT

Critical Mission Parameters:

  • • Starship payload to lunar surface: ~100 tonnes per landing
  • • Orbital refueling: 8-12 tanker flights per lunar mission
  • • Transit time Earth-Moon: ~4.5 days (TLI to LOI)
  • • Target base location: Shackleton Crater rim, 89.9°S
  • • Permanent sunlight availability: 80-90% at crater rim peaks
  • • Water ice reserves: estimated billions of tonnes in PSRs
════════════════════════════════════════════════════════════════════════

MOON TERMINAL ARCHIVES - LUNAR SETTLEMENT PROGRAM DOCUMENTATION

C:\MOON\ARCHIVES> █