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Space Datacenters: Orbital vs Terrestrial Economics

"It might not be rational. But it might be physically possible."

An interactive first-principles cost analysis comparing orbital solar power satellites to terrestrial natural gas for datacenter capacity. Built by Andrew McCalip.

Flask Python License Status


🎯 What Is This?

This is an interactive economic model that asks a simple question: Can you make space-based commodity compute cost-competitive with the cheapest terrestrial alternative?

Instead of hand-waving about "the sun being huge" or "space being big," this tool lets you manipulate the actua 8000 l variables and see what assumptions need to be true for orbital compute to make economic sense.

Key Features

  • Interactive Sliders: Adjust launch costs, satellite hardware costs, specific power, gas prices, PUE, and dozens more parameters
  • Real-Time Calculations: See cost breakdowns, LCOE, and engineering outputs update instantly
  • Thermal Analysis: Full bifacial panel thermal model with equilibrium temperature calculations
  • Propellant & Logistics: LOX/CH4 production energy, Texas grid impact, tanker truck estimates
  • Mobile Responsive: Works on desktop and mobile with adaptive layouts
  • First-Principles Physics: Solar flux, Stefan-Boltzmann radiation, cell degradation, view factors
  • Transparent Math: Formulas are implemented directly in static/js/math.js

📊 The Model

Orbital Solar

  • Starlink V2 Mini heritage bus as reference point
  • Configurable specific power (3-75 W/kg)
  • Launch costs from theoretical floor ($20/kg) to Falcon 9 ($2,940/kg)
  • Cell degradation, GPU failure rates, NRE costs
  • Thermal equilibrium calculations for bifacial panels

Propellant & Logistics (2025 LC-39A Draft EIS)

  • Starship/Super Heavy propellant: 6,750 metric tons per launch (78.3% LOX)
  • Energy requirements: ~0.4 MWh/ton LOX, ~0.8 MWh/ton CH4
  • Texas LOX capacity impact: % of total (~14,500 t/day) and 10% surplus
  • Warning indicators when demand exceeds surplus capacity
  • Tanker truck estimates per launch

Terrestrial (On-Site CCGT)

  • H-Class combined cycle gas turbines
  • 5-bucket capex model: Power Gen, Electrical, Mechanical, Civil/Shell, Network
  • Fuel costs tied to natural gas prices
  • PUE and capacity factor adjustments

Verification

Quick verification scripts live in temp/ and mirror the JavaScript model.

🛠️ Tech Stack

├── Flask 2.2.3          # Web framework
├── Gunicorn 20.1.0      # Production WSGI server
├── Jinja2               # Templating
├── KaTeX                # Math rendering
├── Vanilla JS           # No framework bloat
└── CSS Custom Props     # Theming & responsive design

🚀 Quick Start

Local Development

# Clone the repo
git clone https://github.com/andrewmccalip/thoughts.git
cd thoughts

# Create virtual environment
python -m venv venv

# Activate (Windows)
venv\Scripts\activate

# Activate (Unix/Mac)
source venv/bin/activate

# Install dependencies
pip install -r requirements.txt

# Run the app
python app.py

Visit http://localhost:5000 in your browser.

Docker

# Build the image
docker build -t space-datacenters .

# Run the container
docker run -p 8080:8080 space-datacenters

Visit http://localhost:8080 in your browser.


📁 Project Structure

thoughts/
├── app.py                    # Flask application
├── requirements.txt          # Python dependencies
├── Dockerfile               # Container configuration
│
├── audits/                  # Archived review artifacts
├── static/
│   ├── css/
│   │   └── style.css        # All styling (2400+ lines)
│   ├── js/
│   │   ├── math.js          # Cost model calculations
│   │   └── main.js          # UI controller & interactions
│   └── references.json      # Citation data
│
├── templates/
│   ├── index.html           # Landing page
│   ├── space-datacenters.html  # Main analysis page
│   └── (none)
│
├── reports/                 # Research notes
└── temp/                    # Development scripts

🔧 Configuration

Environment Variables

Variable Default Description
PORT 8080 Server port (Docker)

📐 The Math

Orbital Cost Model

Total Cost = Hardware + Launch + Ops + GPU Replacement + NRE

Hardware = $/W × Initial Capacity (degradation-adjusted)
Launch = $/kg × Total Mass
Mass = Initial Capacity / Specific Power (W/kg)

Thermal Equilibrium

T_eq = [ΣQ_in / (σ·A·ε_tot) + T_space⁴]^¼

Where:
- Q_in = Q_solar + Q_earthIR + Q_albedo + Q_heatloop
- σ = Stefan-Boltzmann constant
- ε_tot = ε_pv + ε_rad (bifacial)

LCOE Comparison

LCOE = Total Cost / Energy Output ($/MWh)

Energy = Capacity × Hours × Capacity Factor


📝 Key Findings

From the analysis (with default assumptions):

  1. It's not obviously stupid — The physics doesn't immediately kill it
  2. The economics are savage — Currently 3-4x more expensive than terrestrial
  3. Vertical integration is everything — Margin stacking kills external procurement
  4. One organization is positioned — SpaceX's integration advantage is the whole ballgame
  5. The math is explicit — Formulas are in static/js/math.js

🤝 Contributing

Found an error in the model? Disagree with an assumption? Good.

  1. Fork the repo
  2. Run the numbers yourself
  3. Open a PR with your corrections
  4. Include sources

The goal is to drag the conversation back to first principles—assumptions you can point at and outputs you can sanity-check.


📜 License

MIT License — Do whatever you want with it.


📬 Contact

Andrew McCalip


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