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Methalox from Titan
The ascent vehicle lifts off at 109 tonnes on 14 tonnes of methane from the sea and 50 tonnes of oxygen from the ice.
See it in the tour: chapter how it survives, shot 7.5.
Two tanks, two sources
The ascent vehicle burns methane and oxygen. Kraken Shore makes both.
The methane comes from the sea. Kraken Mare is a methane-dominated liquid physics, and barges carry it to the plant design. The oxygen comes from water ice. Miners melt it, electrolysis splits it into hydrogen and oxygen, and the town's two small fission reactors supply the power design. The plant has made propellant since 2066, the year the first robotic ascent vehicle reached orbit fiction.
Oxygen is most of the load. One launch takes 14.0 t of methane (35 m³) and 50.3 t of oxygen (46 m³) design. Making the oxygen uses about 57 t of ice physics. The reaction is
CH₄ + 2 O₂ → CO₂ + 2 H₂O
and it balances at 4.0 kg of oxygen per kilogram of methane. The vehicle runs at 3.6 physics. The extra methane keeps the exhaust molecules light, and light molecules leave faster.
The burn
The injector sprays both liquids into a flame physics. A thin flame front turns cold liquid into hot gas, and short-lived radicals, OH and CH, glow blue-violet there physics. Stronger bonds form than break, and the difference is about 800 kJ per mole of methane physics.
Hot gas leaves the nozzle at about 3.4 km/s. That is a specific impulse of 345 s, between the 330 s of sea level and the 360 to 380 s of vacuum physics. As the air thins on the climb, the plume widens and fades to a faint blue-violet above the haze physics.
Storage at 94 K
The tanks stand in air at 94 K. At 94 K and 1.5 bar, liquid methane is stable at ambient temperature and liquid oxygen sits near its boiling point physics. Storage needs far less insulation than on Earth, and no refrigeration for the methane. The vehicle is 26 m long and 4.5 m across design.
Delta-v to orbit
Titan's escape speed is 2.64 km/s, less than a quarter of Earth's physics. A 1,500 km parking orbit, above the bulk of the haze, costs 2.25 km/s ideal physics. Drag and gravity losses add 0.5 km/s, and the design budget of 3 km/s keeps 0.25 km/s of margin design.
At 345 s, 3 km/s takes a mass ratio of 2.427: 109.2 t at liftoff and 45 t of vehicle and payload at the end design. Liftoff thrust is 221 kN, a thrust-to-weight of 1.5 design.
One sea, three customers
The same methane fills the Gateway shuttle, 206.7 t per load (nuclear-thermal). Oxygen goes to the ascent vehicles and to the air indoors. The hydrogen left over from electrolysis becomes reaction mass for the fusion transports design. Saturn exports propellant to the ships that serve it fiction.
Key numbers
| Quantity | Value | Basis |
|---|---|---|
| Reaction | CH₄ + 2 O₂ → CO₂ + 2 H₂O | physics |
| Energy per mole of methane | about 800 kJ | physics |
| Specific impulse (average used) | 345 s | physics |
| Oxygen to methane | 3.6 | physics |
| Methane / oxygen per launch | 14.0 t / 50.3 t | design |
| Ideal delta-v to 1,500 km orbit | 2.25 km/s | physics |
| Design delta-v | 3 km/s | design |
| Liftoff mass / thrust | 109.2 t / 221 kN | design |
| Titan escape speed | 2.64 km/s | physics |
Sources
- JPL, Planetary Satellite Physical Parameters
- NASA, Titan facts
- JPL, PIA19046, Plumbing Coastal Depths in Titan's Kraken Mare