Material transfer interfaces for space vehicles, and associated systems and methods
Material transfer interfaces for space vehicles, and associated systems and methods, are disclosed. A representative system includes a coupling mechanism including a support structure, a latch-arm base movably connected to the support structure, and a latch arm pivotably connected to the latch-arm base. Another representative system includes a service valve portion, a coupling portion configured to receive the service valve portion, and a coupling mechanism for coupling the service valve portion to the coupling portion. The coupling mechanism can include latch arms positioned to pivot between a position in which the latch arms are pivoted outwardly and a position in which the latch arms are pivoted inwardly to capture the service valve portion. The latch arm can be carried by a latch-arm base that translates relative to a support structure of the coupling portion. Material transfer interfaces can include self-aligning ports having faces that engage each other with cup-and-cone structures.
1. A system for transferring material between two spacecraft, the system comprising:
a service valve portion including one or more first ports for transferring material; and
a coupling portion positioned to receive the service valve portion, wherein the coupling portion comprises:
a support structure;
one or more second ports positioned to engage the one or more first ports for transferring material therebetween;
a latch-arm base, wherein the latch-arm base is movable relative to the support structure;
a first actuator positioned to move the latch-arm base relative to the support structure;
a latch arm carried by the latch-arm base, the latch arm being movable relative to the latch-arm base; and
a second actuator positioned to rotate the latch arm relative to the latch-arm base.
2. The system of claim 1 , wherein the coupling portion further comprises one or more sensors, wherein each sensor of the one or more sensors is configured to output a signal.
3. The system of claim 2 , wherein the one or more sensors comprises any one or more of:
a proximity sensor, wherein the signal indicates proximity between the service valve portion and the coupling portion;
a contact sensor, wherein the signal indicates contact between the service valve portion and the coupling portion;
an optical sensor, wherein the signal indicates proximity or contact between the service valve portion and the coupling portion; or
an aliveness sensor, wherein the signal indicates a power state of at least one of the spacecraft.
4. The system of claim 2 , further comprising a controller programmed with instructions that, when executed:
receive at least one of the signals from the one or more sensors; and
in response to the at least one signal, operate the first actuator to translate the latch-arm base and the latch arm to a position in which the latch arm presses the service valve portion against the coupling portion.
5. The system of claim 4 , wherein the controller is further programmed with instructions that, when executed:
operate the second actuator to rotate the latch arm from a first position to a second position in which the latch arm captures the service valve portion.
6. The system of claim 1 , wherein the latch-arm base is connected to the support structure via one or more flexible elements.
7. The system of claim 1 , wherein the latch arm is movable relative to the latch-arm base between a first position and a second position, the system further comprising a spring positioned to bias the latch arm toward the first position.
8. The system of claim 1 , wherein the first actuator comprises a wax motor.
9. The system of claim 1 , wherein the latch-arm base is movable relative to the support structure between a first position and a second position, the system further comprising a spring positioned between the latch-arm base and the support structure to bias the latch-arm base toward the first position.
10. The system of claim 1 , wherein each of the service valve portion and the coupling portion include at least one of (a) a data connector for transferring data between the spacecraft, or (b) a power connector for transferring power between the spacecraft.
11. A system for transferring material between two spacecraft, the system comprising:
a service valve portion including one or more first ports for transferring material; and
a coupling portion positioned to receive the service valve portion, wherein the coupling portion comprises:
a support structure;
one or more second ports positioned to engage the one or more first ports for transferring material therebetween;
a latch-arm base, wherein the latch-arm base is connected to the support structure via one or more flexible elements, and wherein the latch-arm base is movable relative to the support structure;
a first actuator positioned to move the latch-arm base relative to the support structure; and
a latch arm carried by the latch-arm base, the latch arm being movable relative to the latch-arm base.
12. The system of claim 11 , further comprising a controller programmed with instructions that, when executed:
receive at least one signal from at least one sensor; and
in response to the at least one signal, operate the first actuator to translate the latch-arm base to a position in which the latch arm presses the service valve portion against the coupling portion.
13. The system of claim 12 , further comprising a second actuator positioned to rotate the latch arm relative to the latch-arm base, wherein the controller is further programmed with instructions that, when executed:
operate the second actuator to rotate the latch arm from a first position to a second position in which the latch arm captures the service valve portion.
14. A system for transferring material between two spacecraft, the system comprising:
a service valve portion including one or more first ports for transferring material; and
a coupling portion positioned to receive the service valve portion, wherein the coupling portion comprises:
a support structure;
one or more second ports positioned to engage the one or more first ports for transferring material therebetween;
a latch-arm base, wherein the latch-arm base is movable relative to the support structure;
a first actuator positioned to move the latch-arm base relative to the support structure;
a latch arm carried by the latch-arm base, wherein the latch arm is movable relative to the latch-arm base between a first position and a second position; and
a spring positioned to bias the latch arm toward the first position.
15. The system of claim 14 , further comprising a controller programmed with instructions that, when executed:
receive at least one signal from at least one sensor; and
in response to the at least one signal, operate the first actuator to translate the latch-arm base to a position in which the latch arm presses the service valve portion against the coupling portion.
16. The system of claim 14 , further comprising a second actuator positioned to rotate the latch arm relative to the latch-arm base, and a controller programmed with instructions that, when executed:
operate the second actuator to rotate the latch arm from the first position to a second position in which the latch arm captures the service valve portion.
17. A system for transferring material between two spacecraft, the system comprising:
a service valve portion including one or more first ports for transferring material; and
a coupling portion positioned to receive the service valve portion, wherein the coupling portion comprises:
a support structure;
one or more second ports positioned to engage the one or more first ports for transferring material therebetween;
a latch-arm base, wherein the latch-arm base is translatable relative to the support structure;
a first actuator positioned to translate the latch-arm base relative to the support structure; and
a latch arm carried by, and pivotably connected to, the latch-arm base, wherein the latch arm is pivotable between a first pivot position in which the latch arm is pivoted outwardly, and a second pivot position in which the latch arm is pivoted inwardly to capture the service valve portion;
wherein the latch-arm base is translatable relative to the support structure between a first position in which the latch arm allows the service valve portion to move relative to the coupling portion, and a second position in which the latch arm presses the service valve portion against the coupling portion.
18. The system of claim 17 , further comprising a controller programmed with instructions that, when executed:
receive at least one signal from one or more sensors; and
in response to the at least one signal, operate the first actuator to translate the latch-arm base from the first position to the second position.
19. The system of claim 17 , further comprising a second actuator positioned to pivot the latch arm relative to the latch-arm base, and a controller programmed with instructions that, when executed:
operate the second actuator to pivot the latch arm from the first pivot position to the second pivot position.