초록 ▼

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

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).

대표청구항 ▼

What is claimed is: 1. A propellant depot comprising: a utility box having space flight equipment; an exchangeable propellant cartridge system; a propellant cartridge adaptor coupled to said exchangeable propellant cartridge system; a propellant cartridge system docking port coupled to the utility

What is claimed is: 1. A propellant depot comprising: a utility box having space flight equipment; an exchangeable propellant cartridge system; a propellant cartridge adaptor coupled to said exchangeable propellant cartridge system; a propellant cartridge system docking port coupled to the utility box, wherein said propellant cartridge system docking port is removably coupled to said propellant cartridge adaptor and wherein said propellant cartridge system docking port has propellant line couplings for connecting propellant lines in said utility box to propellant lines in said exchangeable propellant cartridge system; at least one docking coupler for coupling to an approaching spacecraft; a controller controlling the transfer of propellant from within said exchangeable propellant cartridge system to said spacecraft; a first plurality of propellant lines which transfer propellant to said at least one docking coupler; and a second plurality of propellant lines, coupled to said exchangeable propellant cartridge system through said propellant cartridge system docking port and coupled to said first plurality of propellant lines, such that propellant passes from the exchangeable propellant cartridge system through the second plurality of propellant lines, through the first plurality of propellant lines, to a docked spacecraft. 2. A propellant depot as in claim 1 wherein said utility box is configured for unmanned flight operation. 3. A propellant depot as in claim 1 wherein said utility box is configured for manned flight operation. 4. A propellant depot as in claim 1 wherein said at least one docking coupler comprises a plurality of docking couplers, said plurality of docking couplers comprising: at least one active propellant coupler; and at least one standby propellant coupler. 5. A propellant depot as in claim 1 wherein said flight equipment comprises elements selected from at least one of flight electronics, cryocooler, communication equipment, helium tank, propellant tank, thrusters, reaction control system equipment, navigation equipment, avionics, power control equipment, cold plates, tracking equipment, and power supply. 6. A propellant depot as in claim 1 further comprising man rated transfer tunnels coupled between said utility box and said at least one docking coupler. 7. A propellant depot as in claim 1 further comprising life support systems coupled to said utility box. 8. A propellant depot as in claim 1 further comprising: a cooling system coupled to said utility box; and a temperature sensor generating a temperature signal indicative of the temperature of a propellant in said exchangeable propellant cartridge system; said controller coupled to said cooling system and said temperature sensor and adjusting temperature of said propellant in response to said temperature signal. 9. The propellant depot of claim 1, further comprising: a first collapsible support stand having a pivoting end and a fixed end with a first docking coupler, of said at least one docking coupler wherein the pivoting end is coupled to the utility box; a second collapsible support stand having a pivoting end and a fixed end with a second docking coupler, of said at least one docking coupler wherein the pivoting end is coupled to the utility box. 10. The propellant depot of claim 9, wherein: each of the first and second support stands have a support leg and a deployment member. 11. The propellant depot of claim 1, wherein the exchangeable propellant cartridge system comprises: a first cylindrical section having a main fuel tank and cartridge propellant lines for carrying fuel to the propellant depot; a second cylindrical section having an oxidizer tank, wherein said second cylindrical section is spaced axially from and connected to said first cylindrical section by a first set of cross-members; an avionics system platform having thrusters, communications devices for communicating with said docking system and a ground system, flight control hardware for guiding said cartridge system mid-flight, and disposal electronics for disposal of the cartridge system wherein said avionics system platform is spaced axially from and connected to said second cylindrical section by a second set of cross-members. 12. The propellant depot of claim 11, wherein said propellant cartridge adaptor comprises: a conical element with a wide end and a narrow end; and propellant lines running along the outside of the conical element; wherein said wide end is attached to the exchangeable propellant cartridge system.