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Helium-3 in Jupiter's Atmosphere: The Fusion Fuel Behind The Gold Rush

A hard-science resource estimate: fusion-fuel demand, where helium-3 comes from and how rich it is, Jupiter's reserves, and the Callisto outpost and Valhalla shipyard.

Overview: solar-wind flux and helium-3 sources from Mercury to Jupiter, grade of each source, Saturn-Callisto-Jupiter supply chain, radiation at Jupiter's moons.

Schematic overview; panels a, b and d computed from Tables 3, 4 and 9, panel c from Tables 1 and 8.

"Until humanity can take stars apart, Jupiter is the inexhaustible source of helium-3." (From A History of Solar System Development, Volume 9: 2145–2245, a fictional book in the film's setting.)

Third-generation fusion burns deuterium and helium-3. In The Gold Rush, the deuterium comes from the clouds of Venus (see Deuterium from Venus). Helium-3 is the other half of the fuel, and the harder half to get. Almost all of the Solar System's ³He is locked inside the Sun. What people can reach is either a thin coating that the solar wind has implanted in the surfaces of airless bodies, or the primordial inventory that the giant planets inherited from the solar nebula.

This article follows that resource from demand to source to grade, then to the outpost and shipyard that the film places on Callisto. The calculations are order-of-magnitude estimates. Each number is labelled as a measurement (physics and spacecraft data that cannot be changed), a model (accepted theory and estimates, such as helium rain in Saturn, Jupiter's interior and the radiation around the Galilean moons) or the setting (engineering extrapolation belonging to the film's fictional world: industrial atmospheric extraction, the Callisto outpost and shipyard, and metastable metallic-hydrogen keels). Calculations are marked as such.

The main findings

Demand. Venus's 90,000 tonnes of deuterium a year must be paired with 135,000 tonnes of ³He. Together they give about 2.5 PW, roughly 6% of humanity's total energy use in the film's era, consistent with Deuterium from Venus.

Surface deposits last only decades. With demand growing 2.5% a year, the Moon's ³He would be used up in about 15 years and Mercury's in about 42.

Jupiter holds about 74 trillion tonnes above the 10 bar level. At the same growth rate that lasts about 665 years, and the planet as a whole holds nearly a million times more.

The grade is three orders of magnitude higher. Jupiter's atmosphere carries about 30 ppm of ³He by mass, about 2,000 times the concentration in lunar soil, and nothing has to be dug. One kilogram of ³He is contained in about 16 Olympic swimming pools of 10 bar gas.

The gravity tax falls on the equipment, not on the fuel. Lifting 1 kg of ³He out of Jupiter's gravity well takes about three millionths of its fusion energy. The real challenge is keeping machines and people working in the depths and in the radiation belts, and that is why the Callisto outpost exists.

Table 1. Resource baseline

ParameterValueBasis
Helium mass fraction of Jupiter's atmosphere0.24Measurement (Galileo probe, 0.234, rounded)
³He/⁴He atom ratio1.66×10⁻⁴Measurement (Galileo probe)
³He mass concentration in Jupiter's atmosphereAbout 30 ppm (2.99×10⁻⁵)Calculation
³He above 10 bar7.4×10¹³ tonnesCalculation
Extraction level10 bar (about 340 K)Setting
Annual demand135,000 t of ³He (paired with 90,000 t of Venusian deuterium)Setting (consistent with Deuterium from Venus)
Recovery of ³He from the processed gas50%Setting
Demand growth2.5% per yearSetting
Outpost and shipyardCallisto, Valhalla basinSetting
Ship keel8.4 million circuits × 12 km × 0.1 cm² of metastable metallic hydrogenSetting (consistent with Jupiter Magnetic Spacecraft)

1. The other half of fusion fuel: helium-3

Fusion of deuterium and helium-3 releases 18.35 MeV. Both products, a helium-4 nucleus and a proton, are charged, so they can be steered by magnetic fields and converted directly into electricity:

$$\mathrm{D}+{}^{3}\mathrm{He}\rightarrow{}^{4}\mathrm{He}\,(3.6\,\mathrm{MeV})+p\,(14.7\,\mathrm{MeV})$$

Table 2. Fusion fuels compared

ReactionEnergy releasedPer kilogram of reactantsEnergy carried by neutrons
D–T17.6 MeV3.4×10¹⁴ JAbout 80%
D–³He18.35 MeV3.5×10¹⁴ JOnly from D–D side reactions, a few per cent
³He–³He12.9 MeVAbout 2.1×10¹⁴ JNone

Measurement: standard nuclear data.

D–³He burns one deuterium atom per ³He atom, a mass ratio of about 2 to 3. The 1,000 extraction tubes on Venus produce 90,000 tonnes of deuterium a year, which therefore need 135,000 tonnes of ³He (calculation):

$$P=\frac{(0.9+1.35)\times10^{8}\,\mathrm{kg}\times3.52\times10^{14}\,\mathrm{J/kg}}{3.156\times10^{7}\,\mathrm{s}}\approx2.5\,\mathrm{PW}$$

That is about 6% of the 42 PW humanity uses in the film's era. The next step, ³He–³He fusion, needs no deuterium and produces no neutrons at all. The price is more ³He: each kilogram of ³He yields only about 2.1×10¹⁴ J in ³He–³He fusion against 5.9×10¹⁴ J in D–³He, so supplying the same 2.5 PW would take about 2.85 times as much, roughly 385,000 tonnes a year (calculation). The bottleneck of the fuel supply is ³He.

2. The solar wind paints helium-3 onto airless bodies

Most of the Solar System's ³He sits inside the Sun. A tiny fraction escapes in the solar wind and is implanted in the surface of bodies that have neither an atmosphere nor a strong magnetic field to protect them. The flux falls with the square of the distance from the Sun:

$$\frac{\Phi_{Mercury}}{\Phi_{Moon}}=\left(\frac{1\,\mathrm{AU}}{0.387\,\mathrm{AU}}\right)^{2}\approx6.7$$

Table 3. Solar-wind deposits

BodyDistance from the SunRelative fluxSurface ³He concentrationInventory (estimate)
Moon1 AU1About 15 ppb (rich regolith)1–2.5 million t
Mercury0.39 AUAbout 6.7Up to about 135 ppbAbout 10 million t

Lunar values are model estimates from regolith samples (published inventories range from under 1 to about 2.5 million tonnes). Mercury's values are a setting estimate; no samples exist.

Mercury's figures are the less certain. The flux there is 6.7 times higher, and more frequent micrometeorite impacts churn the regolith more deeply. But its dayside reaches about 700 K, which drives implanted helium back out of the grains, and its global magnetic field, about 1% of Earth's at the surface, deflects part of the solar wind and funnels it towards the cusp regions near the magnetic poles. The ³He is therefore likely to be concentrated in patches. Spread at 135 ppb through the top 3 m of the whole planet it would come to about 45 million tonnes; the 10 million tonne figure corresponds to an average of about 30 ppb, which allows for that patchiness.

3. The grade of surface deposits

The ³He is concentrated in the top 1–3 m of regolith, and the concentration falls sharply below that. The grade decides how much raw material must be handled per tonne of product:

$$m_{ore}=\frac{1\,\mathrm{t}}{w_{3}}$$

Table 4. Raw material per tonne of helium-3

Source³He mass concentration $w_{3}$Raw materialExcavation
Moon15 ppb67 million t of regolithA square 3.9 km on a side, 3 m deep
Mercury135 ppb7.4 million t of regolithA square 1.3 km on a side, 3 m deep
Jupiter (10 bar)30 ppm33,000 t of atmosphereNo excavation; see Section 7

Calculation; regolith bulk density 1.5 t/m³.

The first problem with the Moon and Mercury is not the grade, however. It is the total.

4. Surface deposits last only decades

Demand will not stay at 135,000 tonnes a year. With 2.5% annual growth, demand in year t is 135,000×1.025ᵗ tonnes, and cumulative consumption after N years is:

$$M(N)=a\left(1.025+1.025^{2}+\cdots+1.025^{N}\right)=a\,\frac{1.025^{N+1}-1.025}{0.025}$$

Table 5. How long each inventory lasts (starting at 135,000 t/yr)

InventoryConstant demandGrowing 2.5%/yrGrowing 2.5%/yr, switched to ³He–³He (2.85× demand)
Moon, 2.5 million tAbout 19 yearsAbout 15 yearsAbout 6 years
Mercury, 10 million tAbout 74 yearsAbout 42 yearsAbout 20 years
Jupiter above 10 bar, 74 trillion tAbout 550 million yearsAbout 665 yearsAbout 620 years

Calculation. The last column assumes the same power is delivered by ³He–³He fusion instead of D–³He.

Cumulative helium-3 demand against the Moon, Mercury and Jupiter inventories: the Moon and Mercury last decades, Jupiter's atmosphere above 10 bar about 665 years.

Figure 1. Cumulative demand against three inventories. a, Cumulative ³He consumed (log scale) starting at 135,000 t a year: constant demand, demand growing 2.5% a year with D–³He fuel, and the same power from ³He–³He fusion (2.85 times the demand). Dashed lines mark the Moon (2.5 million t, shaded: published range), Mercury (10 million t) and Jupiter above 10 bar (74 trillion t); circles mark exhaustion. The whole planet holds nearly a million times more. b, The first 80 years on a linear scale. c, Years until each inventory is used up (Table 5). With exponential growth the Moon and Mercury last only decades, while Jupiter's shallow atmosphere lasts about 665 years. Calculation.

Billions of years of deposits from the Sun would last an industrial civilisation a few decades. Venusian deuterium is different. The Venusian atmosphere holds about 2.5×10¹⁰ tonnes of deuterium, which is not much either, but at 90,000 tonnes a year it still lasts about 280,000 years, far longer than any engineering horizon. The ³He it must be paired with would last only decades on the Moon and Mercury. Humanity can rely on Venus for deuterium, but not on Mercury for helium-3.

The real reserves are in the giant planets, which kept the composition of the primordial nebula.

5. The giant planets: Saturn for hydrogen, Jupiter for helium

Table 6. The four giant planets

PlanetDistance from the SunEscape velocityGravity at 1 barUpper-atmosphere helium mass fractionRole
Jupiter5.2 AU59.5 km/s24.8 m/s²0.24Source of ³He
Saturn9.5 AU35.5 km/s10.4 m/s²About 0.06–0.18 (estimates disagree); below the primordial valueSource of high-purity hydrogen
Uranus19.2 AU21.3 km/s8.9 m/s²About 0.26 (poorly constrained)Too far
Neptune30.1 AU23.5 km/s11.2 m/s²About 0.26 (poorly constrained)Too far

Measurement: NASA planetary fact sheets, Galileo probe and Voyager results. Roles are setting.

The helium mass fraction of the primordial nebula was about 0.27. Saturn's interior is relatively cool, and in a certain range of temperature and pressure helium no longer mixes evenly into metallic hydrogen. It separates into droplets that sink towards the core: helium rain (model). This has stripped much of the helium out of Saturn's upper atmosphere, and the falling droplets turn gravitational energy into heat by friction. Saturn radiates about 1.8 times as much energy as it absorbs from the Sun, and helium rain is thought to supply a large part of the excess.

Helium rain makes Saturn the Solar System's best source of hydrogen: the purest hydrogen, gravity only about 40% of Jupiter's, and much closer than the ice giants. In the setting, the Saturn Materials Bureau supplies hydrogen. The same process leaves Saturn's upper air poorer in ³He. Depending on which helium estimate is used, the grade per tonne of atmosphere is roughly a quarter to three quarters of Jupiter's, and Saturn is nearly twice as far from the inner Solar System. The flying-wing city on Saturn extracts enough ³He from its intake to fuel itself (see the Saturn flying-wing city), but bulk export is left to Jupiter.

Jupiter's interior is hotter and helium rain is weaker there. Its upper atmosphere has lost only a little helium: 0.234 measured by Galileo against about 0.27 in the nebula, a small depletion that, together with the depletion of neon, is itself taken as a sign of some helium rain. It keeps about 0.24 of helium and is also the giant planet closest to the inner Solar System. For helium-3 at industrial scale, Jupiter is the better source.

6. Jupiter's inventory: 74 trillion tonnes

Hydrostatics gives a simple relation: the mass of the gas column above a pressure level equals that pressure divided by the gravitational acceleration. Over the whole planet (calculation):

$$M_{atm}=\frac{pA}{g}=\frac{10^{6}\,\mathrm{Pa}\times6.14\times10^{16}\,\mathrm{m^{2}}}{24.79\,\mathrm{m/s^{2}}}\approx2.48\times10^{21}\,\mathrm{kg}$$

The ³He mass fraction follows from the helium mass fraction and the isotope ratio, since a ³He atom has about 3/4 the mass of a ⁴He atom:

$$w_{3}=Y\times\frac{^{3}\mathrm{He}}{^{4}\mathrm{He}}\times\frac{3}{4}=0.24\times1.66\times10^{-4}\times0.75\approx2.99\times10^{-5}$$
$$M_{3}=w_{3}M_{atm}\approx7.4\times10^{16}\,\mathrm{kg}=7.4\times10^{13}\,\mathrm{t}$$
Jupiter cutaway to scale with a zoom into the atmosphere above 10 bar, about 90 km thick, plus plots of helium-3 above each pressure level and gas volume per kilogram.

Figure 2. Jupiter and the layer where the inventory is counted. a, Cutaway to scale (radius about 70,000 km): cloud bands on the visible half; molecular hydrogen envelope, metallic hydrogen and dilute core in the section (boundaries model-dependent). The atmosphere above 10 bar is about 90 km thick, 0.13% of the radius, too thin to draw to scale. b, Zoom on the outer layer: temperature profile through the Galileo probe values at 1, 5 and 10 bar, cloud decks, and the 10 bar extraction level about 90 km below the 1 bar level. c, ³He in the gas above each pressure level, rising to 7.4×10¹³ t above 10 bar (calculation). d, Volume of gas containing 1 kg of ³He, in Olympic pools: 80 at 1 bar, 26 at 5 bar, 16 at 10 bar (Table 7).

That is only the shallow layer. Taking a helium mass fraction of about 0.27 for the planet as a whole, all of Jupiter's ³He comes to about 6×10²² kg, nearly a million times the shallow inventory (calculation; model-dependent). Growing at 2.5% a year, the shallow layer alone lasts about 665 years. Using up the whole planet would take the technology to dismantle planets, or stars. That is the scale behind the epigraph's "until humanity can take stars apart".

7. Grade: how much atmosphere per kilogram of helium-3

One tonne of ³He is contained in 1/w₃ ≈ 33,500 tonnes of atmosphere. At the setting's 50% recovery, about 67,000 tonnes have to be processed. The volume depends on depth, because Jupiter's atmosphere gets hotter and denser further down:

$$\rho=\frac{pM}{RT},\qquad V=\frac{1\,\mathrm{kg}}{w_{3}\rho}$$

Table 7. Grade at different depths (mean molecular mass 2.3 g/mol)

LevelTemperatureDensity³He atomsAtmosphere containing 1 kg of ³HeOlympic swimming pools
1 bar, ammonia cloud tops165 K (−108 °C)0.17 kg/m³1.0×10²¹ /m³200,000 m³80
5 bar, water cloud layer272 K (−1 °C)0.51 kg/m³3.0×10²¹ /m³66,000 m³26
10 bar, warm deep layer340 K (67 °C)0.81 kg/m³4.8×10²¹ /m³41,000 m³16

Temperatures are measurements (Galileo probe); the rest is calculation. One Olympic pool is taken as 2,500 m³. Volumes are the gas that contains 1 kg; at 50% recovery twice as much must be processed.

There are two reasons to work at 10 bar. The first is grade: each cubic metre holds about 5 times as much ³He as at 1 bar. The second is temperature. At 340 K the gas sits inside the operating window of the metastable metallic-hydrogen alloy described in Metastable Metallic Hydrogen (setting): with a critical temperature of 400 K, the critical field at 340 K is still about 55 T, and a million-tonne installation needs a barrier of about 3.9 eV to last 30 years, below the 4 eV design value. The extraction equipment can use superconducting magnets with no cooling at all.

For 135,000 tonnes a year at 50% recovery, the atmospheric flow is (calculation):

$$Q=\frac{1.35\times10^{8}\,\mathrm{kg/yr}}{0.5\times w_{3}\times3.156\times10^{7}\,\mathrm{s/yr}}\approx2.9\times10^{5}\,\mathrm{kg/s}$$

That is about 290 tonnes, or about 350,000 m³, of 10 bar gas every second, or about 9×10⁹ tonnes a year. For every kilogram of ³He in the gas there are about 8 tonnes of ⁴He and 25 tonnes of hydrogen. The ⁴He is useful as an industrial gas; the hydrogen can be returned to the atmosphere or used on the spot.

8. The gravity tax falls on the equipment, not the fuel

Jupiter has the deepest gravity well in the Solar System. Reaching low orbit from the 1 bar level takes a velocity change of about 29.5 km/s, even after the planet's rotation helps. For a fuel like ³He, however, the gravity tax is almost negligible:

Table 8. Energy ledger per kilogram of helium-3

ItemEnergyShare of fusion energyBasis
Fusion energy of ³He (D–³He, per kg of ³He)5.9×10¹⁴ J1Calculation
Lifting out of the well (cloud tops to Callisto's orbit)About 1.7×10⁹ JAbout 3×10⁻⁶Calculation
Atmospheric processing (1 MJ per kg of gas, 67,000 t of gas)About 6.7×10¹⁰ JAbout 1×10⁻⁴Assumption
Overall energy return—About 8,600Calculation

The fuel's energy density is so high that hauling and refining it cost only a sliver. The real cost falls on what has to go down into the depths: extraction equipment, ships and people. They must work at 2.5 times Earth's gravity, in strong radiation and violent convection, and must be able to go in and out again and again. That sets how Jupiter is developed: build an outpost outside the depths and put manufacturing, maintenance and living quarters there.

9. Choosing the outpost: Callisto

The four large Galilean moons are massive and in stable orbits, natural places to set up. The closer they are to Jupiter, the deeper the gravity well and the stronger the radiation:

Table 9. Jupiter's main moons

MoonOrbital radiusMassOrbital speedUnshielded surface dose (commonly quoted estimates)
Metis128,000 km3.6×10¹⁶ kg31.5 km/sInside the main radiation belt
Amalthea181,000 km2.1×10¹⁸ kg26.4 km/sInside the main radiation belt
Io422,000 km8.9×10²² kg17.3 km/sAbout 36 Sv/day
Europa671,000 km4.8×10²² kg13.7 km/sAbout 5.4 Sv/day
Ganymede1.07 million km1.5×10²³ kg10.9 km/sAbout 0.08 Sv/day
Callisto1.88 million km1.1×10²³ kg8.2 km/sAbout 0.0001 Sv/day

Measurement (orbits and masses, NASA fact sheets); orbital speeds are calculated; doses are rough published estimates.

On Io's surface a lethal dose accumulates within minutes. Living on Ganymede long term needs shielding. Callisto's dose is about 800 times lower than Ganymede's, about 36 mSv a year, outside the range of acute radiation harm. It has other advantages too. Its orbit is the highest of the four, so Jupiter's tides affect it least. It is geologically dead, with no tectonic activity, which suits large fixed installations. Its surface gravity is 1.24 m/s² and its escape velocity only 2.44 km/s, so moving large components on and off the surface is cheap.

10. Valhalla: a shipyard in an impact basin

Callisto is the most heavily cratered body in the Solar System; its surface is a time capsule kept for about 4 billion years. Its largest feature is the Valhalla basin, a multi-ring impact structure about 3,800 km across, like ripples frozen in ice. At its centre is a bright, relatively flat region several hundred kilometres wide, room enough to lay out a large shipyard (setting).

Callisto's environment suits this industrial outpost. The surface temperature is about 80–165 K. At that temperature metastable metallic hydrogen needs a barrier of less than 2 eV to last, so keel material can be stored almost indefinitely, and the cryogenic separation of ³He from ⁴He has a ready cold sink. The ice crust supplies water, oxygen and propellant, and is building material in its own right.

The hazard to avoid is the fields of ice spires, roughly 80–100 m tall. Where dark dust covers the ice, it absorbs sunlight and the ice sublimates, leaving sharp pinnacles behind. For a lander this is a bed of nails, so landing fields and the shipyard have to be sited on flat ground inside the basin and levelled in advance.

11. The superconducting keel: how much metallic hydrogen per ship

The Valhalla shipyard builds the magnetic-lift ships described in Jupiter Magnetic Spacecraft: 12 km long and about 2 km in diameter. The superconducting keel is 8.4 million current circuits. Each circuit has a lift conductor, a return conductor and a shield tube, each 12 km long with a cross-section of 0.1 cm², made of the metastable metallic-hydrogen alloy (density 700 kg/m³). With all three counted (k = 3):

$$m_{keel}=kNLA\rho=3\times8.4\times10^{6}\times1.2\times10^{4}\,\mathrm{m}\times10^{-5}\,\mathrm{m^{2}}\times700\,\mathrm{kg/m^{3}}\approx2.1\times10^{9}\,\mathrm{kg}$$

Table 10. The keel of one ship

ItemValueBasis
Circuits × length × cross-section8.4 million × 12 km × 0.1 cm² (one each of lift conductor, return conductor and shield)Setting
Keel material massAbout 2.12 million tCalculation
Total lift at 10⁴ A per circuit in Jupiter's 4.2 G cloud-top field4.2×10¹¹ N, enough to hold about 17.1 million t (including a 10 million t city payload)Calculation
Minimum manufacturing energy (216 MJ/kg)4.6×10¹⁷ J, about 5.3 days at 1 TWCalculation
FeedstockAbout 2.12 million t of high-purity hydrogen from the Saturn Materials BureauSetting

This links three materials bureaus into one supply chain. Saturn supplies high-purity hydrogen, Callisto forges it into metastable metallic-hydrogen keels, the ships built on those keels descend into Jupiter to extract ³He, and the ³He travels with Venusian deuterium to the fusion reactors of the inner Solar System.

12. Main risks

Table 11. Risks and responses

RiskSourceConsequenceResponse
RadiationJupiter's radiation belts, crossed on every tripEquipment damage, crew doseOutpost on Callisto; magnetic shielding on ships
Landing and terrainIce-spire fieldsLoss of landersSites on flat basin floor, levelled in advance
Supply-chain interruptionHydrogen shipments from Saturn to JupiterLower keel outputReserves on Callisto; by-product hydrogen from Jupiter's atmosphere
Keel material failureLocal overheating, radiation defectsRunaway recombination and heat releaseCold storage on Callisto; barrier acceptance tests before delivery
Demand above forecastEnergy growth above 2.5%Shorter inventory lifetimeExtend extraction to deeper levels

13. From outpost to main mining field

Table 12. The maturity path

StageWhat has to be achievedCriterion (example)Status
0. Resource confirmedHelium and isotope ratio of Jupiter's atmosphereY ≈ 0.24, ³He/⁴He ≈ 1.66×10⁻⁴Measured by the Galileo probe (1995)
1. Outpost establishedBase and landing field on CallistoPermanently crewed, self-sustaining supplySetting
2. Keel production lineSaturn hydrogen forged into metallic hydrogen on CallistoMillions of tonnes a year (about one ship every six months)Setting
3. First shipLaunched from the Valhalla shipyardOne round trip into the depthsSetting
4. Industrial extractionContinuous extraction at 10 barAbout 290 tonnes of atmosphere processed per secondSetting
5. Main mining fieldSupply matched to Venusian deuterium135,000 t of ³He a year, growing with demandSetting

The ³He of the Moon and Mercury is a trail of crumbs left by the Sun. Jupiter's is a whole warehouse left by the primordial nebula. Opening it takes two things: an outpost outside the depths, and a ship that can rise and sink freely within them.

References and calculation basis

  • von Zahn et al. (1998), Helium in Jupiter's atmosphere: results from the Galileo probe helium interferometer experiment, Journal of Geophysical Research 103: helium mass fraction of about 0.234.
  • Mahaffy et al. (1998), Galileo probe measurements of D/H and ³He/⁴He in Jupiter's atmosphere, Space Science Reviews 84: ³He/⁴He ≈ 1.66×10⁻⁴.
  • Seiff et al. (1998), Thermal structure of Jupiter's atmosphere near the edge of a 5-μm hot spot, Journal of Geophysical Research 103: temperatures at each pressure level.
  • Wittenberg, Santarius and Kulcinski (1986), Lunar source of ³He for commercial fusion power, Fusion Technology 10: lunar ³He resources.
  • Conrath et al. (Voyager infrared results for Uranus and Neptune) and later reanalyses: helium abundance in the ice giants.
  • Scienshell, Deuterium from Venus: the deuterium half of the fuel network and the 135,000 t/yr ³He demand.
  • Scienshell, Metastable Metallic Hydrogen: critical temperature, critical field, barrier and manufacturing energy of the metallic-hydrogen alloy (setting).
  • Calculation basis: g = 24.79 m/s² for the atmosphere above 10 bar; mean molecular mass 2.3 g/mol; fusion energies from standard nuclear data; satellite doses are commonly quoted estimates; 2.5% demand growth and 50% recovery are setting.

Appendix A. Principal symbols

Table 13. Symbols

SymbolMeaningSymbolMeaning
YHelium mass fraction$M_{atm}$Mass of atmosphere above a pressure level
$w_{3}$³He mass concentration$M_{3}$³He inventory
ΦSolar-wind fluxQAtmospheric processing flow
aStarting annual demandM(N)Cumulative consumption after N years
ρAtmospheric densityVAtmospheric volume containing 1 kg of ³He

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