Patent ID: 7602349

Claim:
A spacecraft comprising: a spacecraft body; a first phased array coupled to a first side of the spacecraft body; a first reflector coupled to the first side of the spacecraft body; a first deployment couple disposed between the first phased array and the first side of the spacecraft body and coupled to the first phased array and the first side of the spacecraft body, the first deployment couple configured to permit stowing the first phased array parallel to the first side of the spacecraft body; a second deployment couple disposed between the first reflector and the first side of the spacecraft body and coupled to the first reflector and the first side of the spacecraft body, the second deployment couple configured to permit stowing the first reflector parallel to the first side of the spacecraft body; and a first common launch restraint system configured to secure the first phased array and the first reflector to the first side of the spacecraft body using at least one common launch restraint mounting point.