ECLIPSE
Collaborative lunar systems engineering
Digital Engineering Ecosystem
S24 DEE β€” Digital Engineering Ecosystem
1. Build Requirements
2. Mission Network Activation
Activate Systems
Run Graph first to parse the SysML and build the connectivity graph. You can then toggle which modules stay active.
Mission Operations Graph
Module Power flow LOX flow Regolith flow
Graph updates when systems are turned on or off. This is the stakeholder-facing systems view that constrains what the DES is allowed to sequence downstream.
3. Model Submission
Modules
Run Graph first.
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Part Metadata
Select a module on the left.
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Drag & drop a USD/USDA/USDC/USDZ file here
or click to browse
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SysML Metadata
Material
Units
Actions
4. Urban Planning β€” Site Selection & Module Placement
Lunar South Pole Β· Scroll to zoom Β· Drag to pan Β· Click a pin to select
Image: NASA LRO LOLA Β· Data: Jenny Zheng (GT) / NASA SDT / Artemis III studies
β‰₯80% β‰₯75% <75%
Click a site pin to see detailed analysis.
5. Mission Tradespace Selection (DES)
Parameter Controls
Stakeholder changes the assumptions here.
# of regolith rovers 1
Parallel haul capacity to regolith loop.
# of ISRU plants 1
Parallel processing units, shared infrastructure.
FROM URBAN PLANNING
Regolith haul distance β€”
LOX haul distance β€”
Set in Step 4.2 β€” Module Placement
Rover energy (kWh/km/kg) 0.00034
Primary driver for regolith availability.
Rover travel time 5 hr/km
Longer travel delays delivery cadence.
ISRU processing rate 1600 kg/hr
Higher rate increases LOX output.
LOX transport threshold 100 kg
Triggers LOX rover pickup.
Coupled Mission State Network
Node color = system role. Edge label = current flow quantity.
Downstream Consequences
Final simulation outputs at t = 60 hr.
Run the simulation to see results.
6. Simulator