Definition
A rocket propulsion system using liquid methane () as fuel and liquid oxygen (LOX) as oxidizer, chosen by SpaceX as the primary propellant architecture for the Starship system to enable Mars colonization.
- How to read: “The chemical formula for methane, CH4.”
- Meaning: Liquid methane is the fuel; combined with liquid oxygen it burns to produce thrust and can be synthesized on Mars.
Why It Matters
Methalox is the ‘fuel of the future’ for multi-planetary life; by choosing propellant that can be manufactured on Mars, SpaceX has solved the ultimate logistical bottleneck of colonization, ensuring we don’t just visit the red planet, but stay there.
Core Concepts
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Mars ISRU: The primary driver for Methalox is In-Situ Resource Utilization. Methane can be synthesized on Mars using the Sabatier Process:
- How to read: “The reaction of carbon dioxide and four molecules of hydrogen gas yields methane and two molecules of water.”
- Meaning: Martian CO₂ and hydrogen produce methane fuel and water—enabling refueling on Mars.
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Hydrogen vs. Methane: While liquid hydrogen () has a higher specific impulse (), liquid methane is denser (smaller tanks), easier to store (boils at –259°F vs –423°F), and does not cause hydrogen embrittlement in metals.
- How to read: “The liquid hydrogen; the specific impulse.”
- Meaning: Liquid hydrogen has higher specific impulse but is harder to store; methane trades some for practicality and Mars producibility.
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Engine Architecture: The Raptor engine uses a full-flow staged combustion cycle, which is highly efficient when burning methane.
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Clean Burning: Methane burns cleaner than kerosene (RP-1), producing significantly less soot (coking), which is essential for rapid engine reuse without refurbishment.