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 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.