Titan 2100

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Radiators: throwing heat away

Every reactor in the Saturn fleet makes more heat than power, and the only way to get rid of the rest is to shine it into the dark.

See it in the tour: chapter long passage, shot 0.3.

Light is the only way out

Concordia teaches the basics: why a vacuum is a thermos and where a habitat's power and heat go. This page does the arithmetic for three machines at Saturn.

Space has no air to carry heat away. A surface sheds heat only as thermal light, and the power a flat panel radiates is its emissivity times σT⁴ per side physics. Here σ is the Stefan-Boltzmann constant, 5.67 × 10⁻⁸ W/m²K⁴. One square metre of black surface radiates 3.5 kW at 500 K and 117.6 kW at 1,200 K physics. The same panel is 33 times better at the higher temperature.

250 K500 K1,000 K1,500 K100 m²1,000 m²10,000 m²100,000 m²1,000,000 m²Long Passage: 10,630 m² at 1,200 Krejecting 2.12 GWGateway: 941 m² at 500 Krejecting 6.00 MWCargo tug: 790 m² at 500 Krejecting 4.76 MWthe same heat at 500 K: 352,544 m²Radiator area, two-sidedRadiator temperatureArea = heat ÷ (2 × emissivity × σ × T⁴). Emissivity 0.85 on the vehicle sheets, 0.9 on the Gateway sheet. Both axes logarithmic.
Radiated power grows with the fourth power of temperature, so heat that would need 352,544 m² of radiator at 500 K needs 10,630 m² at 1,200 K: 33 times less. That is why the fusion ship's radiators are streams of hot droplets. physics design challenge

Why there is so much heat

A heat engine turns only part of a reactor's heat into power. The tug's reactor makes 5.8 MW of heat and 1.74 MW of electricity, so most of the heat has to go somewhere physics. See Reactors and heat on Titan. On Titan that heat is useful. In space it is waste.

Three radiators in the fleet's data show the scale design.

At 500 K that 2.1 GW would need 352,544 m². Running hot is what keeps the ship a ship physics.

Why droplets

A solid panel at 1,200 K needs structure, plumbing and coolant lines, and a micrometeoroid can puncture it. A liquid-droplet radiator drops the panel. It sprays a sheet of droplets, each under about 100 microns, across a gap in vacuum. The droplets radiate as they fly, and a collector catches them and pumps them back to the heat exchanger physics. Mattick and Hertzberg described it in 1981. They argued it could weigh much less than heat-pipe panels and be less vulnerable to micrometeoroids, with the droplet generator, collector, heat exchanger and pump making up most of the mass physics.

A small membrane room on a grown lattice, one shielded port aft toward the radiators.
The engine gallery. A small membrane room on a grown lattice, one shielded port aft toward the radiators.

The ship carries four wings of droplet sheets, each 150 m long and 17.7 m across challenge. Hot droplets glow, so the radiators are the part of the ship that shows its power. The engine gallery's view port looks out on them design. They also set the width of the shield, because they are the nearest large structure behind it. See Shadow shields and neutrons.

Key numbers

QuantityValueBasis
Radiated power per m² per side, black surface, 500 K3.5 kWphysics
Radiated power per m² per side, black surface, 1,200 K117.6 kWphysics
Gateway: heat / temperature / area6 MW / 500 K / 941 m²design
Tug: reactor heat / electricity5.8 MW / 1.74 MWphysics
Tug: area at 500 K790 m²design
Long Passage: heat rejected2.1 GWchallenge
Long Passage: area at 1,200 K10,630 m²challenge
Long Passage: area if run at 500 K352,544 m²physics
Radiator wings4, 150 m by 17.7 mchallenge
Emissivity, two-sided panels0.85 (fleet sheets), 0.9 (Gateway)design

Sources