Lenth: 2.72km
Wet mass, with cargo: 406,000 tonnes
Dry mass, clean: 210,000 tonnes
Dry mass, with crew and passengers: 240,000 tonnes
Payload: 110,000 tonnes
Fuel, liquid deuterium: 620 tonnes
Fuel, LH2: 55,180 tonnes
D/H mass ratio: 1:89
Fuel consumption, outbound, cargo: 22,000 tonnes
Fuel consumption, inbound, crew and passengers: 34,000 tonnes
Fusion power: 12TW
Power-to-Mass ratio, clean: 57.1kW/kg
Effective power for propulsion: 4TW
Isp, pure fusion: 468,000s
Isp, afterburner: 49,000s
Afterburner thrust: 1,670 tonnes
TWR, outbound, loaded: 4.11mG
TWR, inbound: 6.09mG
Outbound Δv budget: 26,740m/s
Inbound Δv budget: 63,590m/s
Usable Δv, fully loaded(110,000 tonnes payload): 71,200m/s
Usable Δv, crew and passenger only: 100,660m/s
Wet mass for Europa cargo mission: 340,000 tonnes
Cargo capacity for heavy element: 90,000 tonnes
Total volume of main liquid tank: 5,475,300 cubic meters
Usable volume of of main liquid tanks: 4,079,600 cubic meters
Energy total loss (waste heat): 53.5%
Energy loss of bremsstrahlung radiation: 13.1%
Energy loss of 2.54MeV neutron (from D-D fusion): 33.6%
Energy loss of 14.1MeV neutron (from D-T fusion): 6.8%
Total waste heat: 6.42TW
Blocked by the structure: ~10%
Grazed by the structure: ~50%
Remaining waste heat load: 330GW
Blade shield maximum temperature: ~2,500K
Blade shield capacity: ~37GW
Radiator maximum temperature: ~1,700K
Dimension of radiator: 2×2×150×1,100m, total area 660,000 square meters
Radiator capacity:313GW (20GW capacity as redundancy)
Axial Magnetic Field Density:~20T
β Ratio:≈0.5
Fusion Average Ion Temperature:~272.6keV
Equilibrium Electron Temperature:~149.2keV
Average Electron Density:1.18*10^21 m^-3
Average Plasma Density:3.82*10^-6 kg•m^-3
Fusion Plasma Volume:>112000 m^3
Fusion Chamber Length:1100m
Fusion Chamber Typical Cross Section:101m^2
Magnetic Energy Held in Coils:>17.7TJ’
Framework stain energy: 1MJ/kg, coil framework mass: ~20,000 tonnes