Abstract: A spacecraft docking system configured to permit the docking of a spacecraft to a target object is provided. The docking system includes a grapple and docking interface, which is mounted on the target object. The grapple includes a body coupled to the spacecraft and at least one latching wing coupled to the body. The at least one latching wing is movable between a retracted position and an extended position, and configured to move into the extended position and latch onto the docking interface when the grapple is inserted therein.

Abstract: Methods and systems for assembling spacecraft in space are provided. A modular spacecraft comprises a plurality of spacecraft modules, wherein each spacecraft module includes one or more of bonding posts and receiving plates mounted to an exterior surface each spacecraft module, wherein the one or more bonding posts and receiving plates are adapted to form one or more of, an electro-weld bond and an adhesive bond, with the one or more receiving plates.

Abstract: Satellites are launched to a first orbit on a launch rocket. The satellites are connected together, forming a satellite cluster, that is propelled from the first orbit to a higher mission orbit by thrustors on each satellite. The satellite cluster is formed so that satellite cluster rotation from aerodynamic drag on the individual satellites is minimized. The thrustors are sequenced to control satellite cluster attitude during the transition to the second altitude. At the second altitude, the satellites are separated from the satellite cluster and propelled to their mission orbits using their own thrustors and attitude system.