FIELD: spacecraft.
SUBSTANCE: proposed method includes topping up of propellant tank with pressurizing gas and transfer of propellant components from emptied tank into receiving tank. Amount of propellant transferred from emptied tank is determined by ratio depending on pressurizing gas temperature at beginning and end of propellant transfer and temperature and pressure in gas space of emptied propellant tank at end of process.
EFFECT: improved reliability of spacecraft topping up system, simplified design of propellant tank and reliability of its sealing.
1 dwg
Authors
Dates
2005-09-27—Published
2003-06-24—Filed