A high capacity satellite having a launch configuration in which one or more antenna reflectors may be stored forward of a forward surface of the spacecraft and an on-orbit configuration in which a reflector boom may be extended forward and rotated to place the one or more antenna reflectors outboard of the spacecraft main body and further forward of the forward surface of the spacecraft. The adaptation circuitry may include summation node circuitry for processing an error value associated with the data signal. The application identification tag identifies a creator application program, which was used to create the electronic file and is operable for editing the content data of the electronic file. The rate of the feed roller is determined based on the rate of the conveyance roller and an allowable amount of a loop formed by a rate difference between the two rollers.