US 11,053,027 B2
Space-based gas supply system
John Behrens, Torrance, CA (US); Craig Alan Christy, Seal Beach, CA (US); Andrew Ian Mactavish, Palos Verdes Estates, CA (US); and Kevin Nemeth, Redondo Beach, CA (US)
Assigned to The Boeing Company, Chicago, IL (US)
Filed by THE BOEING COMPANY, Chicago, IL (US)
Filed on Oct. 1, 2018, as Appl. No. 16/148,870.
Prior Publication US 2020/0102098 A1, Apr. 2, 2020
Int. Cl. B64G 1/10 (2006.01); B67D 7/02 (2010.01); B67D 7/36 (2010.01); B64G 1/64 (2006.01)
CPC B64G 1/1078 (2013.01) [B67D 7/0294 (2013.01); B67D 7/36 (2013.01); B64G 1/646 (2013.01)] 20 Claims
OG exemplary drawing
1. A method of supplying a receiving tank of a receiving spacecraft with a supply gas, said method comprising:
coupling a transfer line of a supply spacecraft in flow communication with the receiving tank on the receiving spacecraft, wherein the transfer line is coupled to a transfer tank disposed on the supply spacecraft, wherein the transfer tank holds a transfer quantity of the supply gas, wherein the supply spacecraft includes (i) a heating system coupled in thermal communication with the transfer tank and (ii) a transfer valve operatively coupled to the transfer line;
activating the heating system while the transfer valve is closed such that a pressure of the transfer quantity of the supply gas is increased; and
opening the transfer valve, wherein a difference between the increased pressure of the supply gas in the transfer tank and a pressure in the receiving tank causes a portion of the transfer quantity of the supply gas to flow through the transfer line to the receiving tank.