Spacecraft systems and methods
Embodiments provide a spacecraft airlock system. Embodiments provide a method and apparatus for attaching space exposed payloads to a space station.
1. A spacecraft enclosure, comprising:
a berthing mechanism positioned around one end of the enclosure for selectively engaging the enclosure with a space station or with a transportation vehicle for transporting the enclosure proximate to the space station;
a cylindrical sidewall adjoining the berthing mechanism of the enclosure;
an endwall adjoining the cylindrical sidewall, opposite the berthing mechanism of the enclosure;
an attachment mechanism positioned on the cylindrical sidewall or the endwall, and configured for releasably attaching vacuum exposed payloads to an exterior surface of the enclosure; and
a grappling fixture positioned on the cylindrical sidewall or the endwall, and configured for engaging a robotic grappling arm of the space station for robotic manipulation of the enclosure, the grappling fixture being configured to engage the robotic grappling arm for disengaging the enclosure from the transportation vehicle in preparation for controllably positioning the enclosure on the space station.
2. The spacecraft enclosure of claim 1 , wherein the grappling fixture comprises a grappling fixture from the group consisting of a power/video grappling fixture, a flight releasable grappling fixture, and similarly functioning grappling fixtures capable of robotic control from a robotic control circuitry.
3. The spacecraft enclosure of claim 1 , wherein the enclosure is an airlock.
4. The spacecraft enclosure of claim 3 , wherein the berthing mechanism of the enclosure engages the airlock with the space station at an active common berthing mechanism of the space station for receiving pressurized air from inside the space station.
5. The spacecraft enclosure of claim 3 , wherein said airlock forms a pressurized volume accessible by crew.
6. The spacecraft enclosure of claim 3 ,
wherein said airlock forms a pressurized volume accessible by crew, said pressurized volume accessible through a single hatch.
7. The spacecraft enclosure of claim 3 ,
wherein said airlock forms a pressurized volume accessible by crew without the use of a hatch to perform the airlock function.
8. The spacecraft enclosure of claim 3 ,
wherein said enclosure permits operation of electrical, data, coolant, and other operational systems using the closable opening.
9. The spacecraft enclosure of claim 1 ,
wherein said robotic grappling arm operates responsive to direct control from an operator directing the engagement of the enclosure.
10. The spacecraft enclosure of claim 1 , further comprising a closable opening on the surface of the endwall, wherein the closable opening permits access from the exterior of the enclosure to the interior of the enclosure.
11. A method for attaching an enclosure to a spacecraft, comprising the steps of:
engaging a berthing mechanism positioned around one end of the enclosure to a space station, the enclosure comprising a cylindrical sidewall adjoining the berthing mechanism and an endwall adjoining the cylindrical sidewall, opposite the berthing mechanism of the enclosure;
attaching vacuum exposed payloads to an exterior surface of the enclosure using an attachment mechanism, wherein the at least one attachment mechanism is positioned on the said cylindrical sidewall or said endwall;
engaging a robotic grappling arm to a grappling fixture positioned on the cylindrical sidewall or the endwall for robotic manipulation of the enclosure;
engaging the enclosure with a transportation vehicle for transporting the enclosure proximate to the space station; and
engaging the grappling fixture of the enclosure with the robotic grappling arm of the space station for disengaging the enclosure from the transportation vehicle in preparation for controllably positioning the enclosure on said space station.
12. The method of claim 11 , further comprising the step of robotically controlling the grappling fixture as a grappling fixture from the group consisting of a power/video grappling fixture, a flight releasable grappling fixture, and similarly functioning grappling fixtures.
13. The method of claim 11 , wherein the enclosure is an airlock.
14. The method of claim 13 , further comprising the step of engaging via the berthing mechanism of the enclosure, the airlock with the space station at an active common berthing mechanism of the space station for receiving pressurized air from inside the space station.
15. The method of claim 14 , further comprising the step of forming a pressurized volume accessible by crew using the airlock.
16. The method of claim 14 , further comprising the step of accessing a pressurized volume formed by the airlock through a single hatch.
17. The method of claim 14 , further comprising the step of accessing a pressurized volume formed by the airlock through a single hatch without the use of a hatch to perform the airlock function.
18. The method of claim 13 , operating electrical, data, coolant, and other operational systems associated with the enclosure using the closable opening.
19. The method of claim 11 , further comprising the step of operating the robotic grappling arm responsive to direct control from an operator directing the engagement of the enclosure.
20. The method of claim 11 , further comprising a closable opening on the surface of the endwall, wherein the closable opening permits access from the exterior of the enclosure to the interior of the enclosure.