STARBASE SIM

Starship Flight Cadence & Pad Turnaround Simulator

Quantitative launch throughput model grounded in NSF Starbase operations
Scenarios:
Annual Cadence -- -- days avg interval
Annual LEO Payload -- Metric tons to LEO (150t/flight)
Primary Bottleneck -- --
Campaign Span -- For 14 flights
Operational Controls
Starbase Pad Layout
14
14 d
18 d
12 d
10 d
State: Active | Active Pads: 1 | Pacing Limit: 24 days
Multi-Flight Launch Campaign Timeline (Gantt)
Stage Prep
Cryo/Static Fire
Pad Recycle
FAA Clearance
Launch Target
Flight Manifest & Bottleneck Ledger
Flight # Assigned Pad Stack Ready Pad Available Licensing Clear T-0 Net Day Critical Path Constraint
Starbase Operational Context: NSF reporting highlights Pad 2 supporting active flights (e.g. Flight 14 in September) while Pad 1 undergoes reconstruction for 2027 dual-pad operations. Turnaround is bounded by the max of vehicle stage readiness, pad refurbishment, and FAA regulatory pacing.
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