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

17

Capacity

50 t per tank

 

Diameter

5 m

 

Length

10 m to 20 m

 

Fluids

hydrogen, methane, oxygen

11,114

Storage time

6 month to 12 month

20

Acceleration

From microgravity to high-g

8,17

Pressure

100 kPa to 350 kPa

8,11

Conditioning

Autogeneous pressurization

8,11,13,115

Heat flux

50 W m2 to 100 W m2

26,116

Transfer rate

0.15 kg s1 to 4.4 kg s1

117,118

Wall material

Aluminum

25

  1. The data have been compiled from different sources.