发明名称 Space depot for spacecraft resupply
摘要 A propellant depot (40, 150) includes a utility box (42, 42') that has space flight equipment. A propellant cartridge adaptor (95) is coupled to the utility box (42, 42') and to an exchangeable propellant cartridge system (41). The propellant depot (40, 150) also includes a docking adaptor (44) for coupling to an approaching spacecraft (24). A controller (66) controls the transfer of propellant from within the exchangeable propellant cartridge system (41) to the spacecraft (24). A method of providing propellant to a spacecraft in space includes launching an orbital propellant depot (40, 150) into space. The spacecraft is docked to the orbital propellant depot (40, 150) in space. Propellant is transferred to the spacecraft. The spacecraft is separated from the orbital propellant depot (40, 150).
申请公布号 US7575200(B2) 申请公布日期 2009.08.18
申请号 US20050162333 申请日期 2005.09.07
申请人 THE BOEING COMPANY 发明人 BEHRENS JOHN W.;CHANDLER FRANK O.;CRONICK JEFFREY J.
分类号 B64G1/00;B64G1/64 主分类号 B64G1/00
代理机构 代理人
主权项
地址