Table 1 Rough order of magnitude parameters for propellant depots in space
From: Cryogenic propellant management in space: open challenges and perspectives
Depot type | dual fluid, 6 to 8 tanks | |
Capacity | 50 t per tank | |
Diameter | 5 m | |
Length | 10 m to 20 m | |
Fluids | hydrogen, methane, oxygen | |
Storage time | 6 month to 12 month | |
Acceleration | From microgravity to high-g | |
Pressure | 100 kPa to 350 kPa | |
Conditioning | Autogeneous pressurization | |
Heat flux | 50 W m2 to 100 W m2 | |
Transfer rate | 0.15 kg s1 to 4.4 kg s1 | |
Wall material | Aluminum |