SWOVEEWORLD / LUNAR SURFACE LOOP
MOON / CONCEPT SIMULATION / MISSION LAB 02

TURN SOIL
INTO SHELTER.

Choose what the fleet should make, how it stays powered and how dry regolith becomes useful infrastructure. Then run the scenario and confront the first modeled hold.

NO BULK WATERNO PORTLAND CEMENTIMPORTED PRESSURE LINER
S01
R01
CONCEPT VISUAL · NOT FOR FABRICATION
MISSION CONFIGURATOR

SCOOP → SCREEN → COMPACT → FUSE → INSPECT.

Every number below is a transparent synthetic planning assumption—not flight data, a construction forecast or a product specification.

01 / WHAT TO BUILD
02 / POWER ARCHITECTURE
03 / FORMING PROCESS
SELECTED MISSIONDust-hardened padLOW, HORIZONTAL FUSED SKIN
MODELED CLOCK130.4 H24.0 h excavation + 106.4 h forming
PROCESS ENERGY1489 KWHDoes not include habitat systems, launch or surface-grid losses
POWER MARGIN26.0 KWConfiguration delta, not qualified reserve
MISSION GATERELEASERelease only to a physical coupon test
MODELED EXPEDITION EVENTDIELECTRIC DRIFT — a witness coupon heats unevenly; slow the scan and re-qualify the feed lot.

Build the witness coupon, inspect porosity and accept or reject the lot before scaling.

WHAT THE GAME IS TEACHING

THE RIGHT ANSWER CAN BE
STOP AND TEST.

Local output

Loose compacted shielding, fused pads, pavers and protective compression forms are plausible research targets.

Imported essentials

Power, electronics, wear parts, reinforcement and the certified pressure liner remain delivered hardware.

Unresolved

Vacuum heating scale-up, thermal cycling, full-structure QA, dust endurance and independent structural acceptance.