Integrated storage and transfer system and method for spacecraft

Fluent material handling – with receiver or receiver coacting mea – With testing or weighing receiver content

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141 4, 141 11, 244135C, 137583, 137382, B65B 104, F16K 2400

Patent

active

057494029

ABSTRACT:
A method of loading propellant into a spacecraft that comprises storing and transferring propellant in a portable propellant loading tank, temperature conditioning and helium saturating the propellant in the propellant loading tank, transferring the loading tank to a launch site, coupling the loading tank to the propellant storage tank, and pressurizing the portable propellant loading tank to transfer the propellant to the propellant storage tank in the spacecraft. The method may further comprise weighing the propellant loading tank during propellant transfer, venting the propellant storage tank in the spacecraft to a receiver tank, and weighing the receiver tank during propellant transfer. The amount of propellant transferred to the propellant storage tank is equal to the difference between the measured weights of the respective loading and storage tanks.

REFERENCES:
patent: 3490205 (1970-01-01), Hauser
patent: 4609169 (1986-09-01), Schweickert et al.
patent: 4768347 (1988-09-01), Manz et al.
patent: 5499656 (1996-03-01), Stotelmyer et al.
Debus, K. "Abschusseinrichtungen fur raumfahrzeuge," VDI Zeitschrift , vol. 107, No. 28, Oct. 1965, pp. 1350-1362.

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