Spacecraft interface module for enabling versatile space platform logistics support
Systems and methods to deliver crew, cargo and other logistics services to space platforms. In one embodiment, a rendezvous and docking vehicle (RDV) comprises two docking mechanisms coupled to the RDV body. A pressurizable passageway connects the docking mechanisms. In one embodiment, the two docking mechanisms are different. An alternative embodiment comprises docking mechanisms which are the same. Also included is a flight control system. The flight control system may vary between embodiments, being autonomous, automated, or remotely controlled (e.g., remote pilot). One embodiment can also include a docking control system in the RDV. A propulsion system is coupled to the RDV in some embodiments, and the RDV may be augmented by a mated spacecraft's propulsion system in other embodiments. The mated spacecraft's propulsion system may even be under the control of the RDV.
1. A reusable rendezvous and docking vehicle (RDV) comprising:
a first docking mechanism configured to mate with a first target spacecraft;
a second docking mechanism configured to mate with a second target spacecraft;
an RDV body coupling the first docking mechanism to the second docking mechanism, wherein the RDV body has a passageway from the first docking mechanism to the second docking mechanism, wherein the RDV body comprises a first module and a second module, wherein the first module is configured to separably mate with the second module, and wherein the first docking mechanism is coupled to the first module and the second docking mechanism is coupled to the second module; and
a flight control system mounted in the RDV and configured to maneuver the RDV.
2. The RDV of claim 1 , wherein the passageway is configured to be pressurized.
3. The RDV of claim 1 , further comprising a propulsion system mounted on the RDV body and configured to be controlled by the flight control system.
4. The RDV of claim 1 , further comprising a docking control system residing in the RDV.
5. The RDV of claim 1 , wherein the flight control system is an automated flight control system.
6. The RDV of claim 1 , wherein the flight control system is an autonomous flight control system.
7. The RDV of claim 1 , wherein the flight control system is configured to enable remote piloting of the RDV.
8. The RDV of claim 1 , wherein the first and second modules each comprise a module body, and the module body of the first module and the module body of the second module have substantially the same configuration.
9. The RDV of claim 1 , wherein the first docking mechanism is a first type of docking mechanism, and the second docking mechanism is a second type of docking mechanism, wherein the first type is different from the second type.
10. The RDV of claim 1 , further comprising a thruster control system residing in the RDV configured to control one or more thrusters which are coupled to the first or second spacecraft.
11. The RDV of claim 1 , further comprising a grapple fixture coupled to the RDV body.
12. The RDV of claim 1 , further comprising a manipulator coupled to the module body and configured to manipulate one of the first spacecraft and the second spacecraft.
13. The RDV of claim 12 , wherein the manipulator comprises two robotic arms.
14. The RDV of claim 1 , wherein the RDV is configured to undock itself from the first target spacecraft and the second target spacecraft, and to dock the first target spacecraft directly with the second target spacecraft.