Abstract: A modular service interface is provided. The modular service interface includes separable first and second halves, one or more alignment features, a connector interface and one or more electropermanent magnet modules, connector interface configured to mate the first and second halves when activated and allow the first and second halves to be separated when inactivated. The modular service interface includes no mechanical actuators to retain the first half to the second half.

Abstract: A capture interface is provided. The capture interface is configured to be rigidly affixed to an external surface of a recovery object and captured by a capture device. The capture interface includes a matte ferromagnetic surface of flat disposition and geometric outline, configured to facilitate capture by the capture device. The ferromagnetic surface includes a capture interface identifier.

Abstract: A fluid transfer interface is provided. The fluid transfer interface includes one or more of first and second interface portions. The first interface portion includes a first portion of a fluid connector and one or more ferromagnetic surfaces. The second interface portion includes an extendable second portion of the fluid connector and one or more electropermanent magnets, laterally disposed around the second portion of the fluid connector, configured to be magnetized or demagnetized in unison. The one or more electropermanent magnets are further configured to provide attraction force to the one or more ferromagnetic surfaces when magnetized and couple the first interface portion to the second interface portion and provide no attraction force to the one or more ferromagnetic surfaces when demagnetized and allow the first interface portion to be decoupled from the second interface portion.

Abstract: An electropermanent magnet array is provided. The electropermanent magnet array includes one or more of a plurality of electropermanent magnets, arranged in a parallel fashion, a plurality of switching circuits, each switching circuit coupled to a different electropermanent magnet of the plurality of electropermanent magnets, and a control circuit, coupled to the plurality of switching circuits. The control circuit is configured to receive commands to control the plurality of switching circuits to demagnetize the plurality of electropermanent magnets, magnetize the plurality of electropermanent magnets to produce a first magnetic field with a strength and an attraction distance and magnetize the plurality of electropermanent magnets to produce a second magnetic field with a lower strength and greater attraction distance than the first magnetic field.

Abstract: An electropermanent magnet array is provided. The electropermanent magnet array includes one or more of a plurality of electropermanent magnets of common length, arranged in a parallel fashion, and a planar pole piece, coupled to the first ends of the plurality of electropermanent magnets. Each electropermanent magnet includes a first and a second end opposite the first end.

Abstract: An electropermanent magnet array is provided. The electropermanent magnet array includes one or more of a plurality of electropermanent magnets of common length, arranged in a parallel fashion, and a planar pole piece, coupled to the first ends of the plurality of electropermanent magnets. Each electropermanent magnet includes a first and a second end opposite the first end.

Abstract: A modular service interface is provided. The modular service interface includes separable first and second halves, one or more alignment features, a connector interface and one or more electropermanent magnet modules, connector interface configured to mate the first and second halves when activated and allow the first and second halves to be separated when inactivated. The modular service interface includes no mechanical actuators to retain the first half to the second half.

Abstract: A capture interface is provided. The capture interface is configured to be rigidly affixed to an external surface of a recovery object and captured by a capture device. The capture interface includes a matte ferromagnetic surface of flat disposition and geometric outline, configured to facilitate capture by the capture device. The ferromagnetic surface includes a capture interface identifier.

Abstract: A device for non-cooperatively capturing an object is provided. The device includes a boom having a fixed end coupled to a structure and a free end. The boom also includes boom deployers for moving the fixed end of the boom relative to the structure. The device also includes a capture head, coupled to the free end of the boom, and a control apparatus. The control apparatus controls the boom deployers and capture head to move the capture head in close proximity to the object. The control apparatus moves the capture head in closer proximity to the object if the capture head is not close enough to the object to capture the object. The control apparatus minimizes forces applied to the object, and activates a non-cooperative capture device. The non-cooperative capture device makes initial contact with the object, establishes intimate contact with the object, and captures the object.

Abstract: A method for delivering a payload to a space facility is provided. The method includes detecting the relative position and velocity of a launch vehicle stage, the launch vehicle stage including the payload and one or more thrusters. The method also includes providing guidance information to the launch vehicle stage. The launch vehicle stage does not include a relative navigation system. In response to receiving the guidance information, the method further includes activating one or more thrusters corresponding to the guidance information, and guiding a capture head of a boom into capture proximity to the payload. One end of the boom is coupled to the space facility and the other end of the boom is coupled to the capture head. The method also includes capturing the payload, removing any residual relative velocity of the payload relative to the space facility, and moving the captured payload to the space facility.

Abstract: A device for non-cooperatively capturing an object is provided. The device includes a boom having a fixed end coupled to a structure and a free end. The boom also includes boom deployers for moving the fixed end of the boom relative to the structure. The device also includes a capture head, coupled to the free end of the boom, and a control apparatus. The control apparatus controls the boom deployers and capture head to move the capture head in close proximity to the object. The control apparatus moves the capture head in closer proximity to the object if the capture head is not close enough to the object to capture the object. The control apparatus minimizes forces applied to the object, and activates a non-cooperative capture device. The non-cooperative capture device makes initial contact with the object, establishes intimate contact with the object, and captures the object.