Orbital Location Trade Analysis

Multi-objective Monte Carlo analysis to determine optimal orbital depot locations. Compare orbital positions from lunar NRHO to Mercury orbit across cost, risk, and capability objectives.

Trade Parameters

8 locations selected

1.5 MW 3.25 MW 5.0 MW
4 km/s 8 km/s 12 km/s
10 55 100
Cost (delta-V) 40%
Risk (stability) 30%
Capability (power/comm) 30%

Location Overview

Near Rectilinear Halo Orbit 1 AU
Sun-Earth L1 0.99 AU
Sun-Earth L4 (Leading) 1 AU
Sun-Earth L5 (Trailing) 1 AU

+4 more...

Pareto Frontier

Cost Score vs Capability Score (point size = stability/risk)

Run analysis to see Pareto frontier

Analysis Results

Configure the trade parameters and run the analysis to see results.

Analysis Methodology

This multi-objective Monte Carlo simulation evaluates candidate orbital locations across three weighted objectives: cost (delta-V requirements), risk (orbital stability), and capability (solar power availability, communication latency).

  • Cost Score: Based on delta-V from Earth and to feedstock sources. Lower delta-V = higher score.
  • Risk Score: Based on orbital stability class and station-keeping requirements. Dynamically stable orbits score highest.
  • Capability Score: Combines solar flux (power generation), communication latency, and thermal feasibility for manufacturing operations.
  • Pareto Frontier: Identifies non-dominated solutions where no single location is better in all objectives simultaneously.

Note: Locations closer to the Sun offer more power but face thermal management challenges. L4/L5 points offer stability but longer communication delays.

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