Abstract: An antenna mounting system for use with recreational vehicles and boats as well as stationary objects. The system includes a pedestal securable to the recreational vehicle and an antenna head containing an antenna element and securable to the pedestal. The pedestal has an upstanding male portion slidably receivable in a mating, female portion of the antenna head. In assembling the system, the male and female portions are first axially aligned and then moved axially toward each other to a predetermined, operating position where they are snapped together in a locking engagement. Anti-rotation structure including one or more pairs of mating, channels and protuberance is also provided to prevent the pedestal and antenna head from being rotated relative to each other about their aligned axes (and the coaxial cable running through them from being twisted) as they are moved together to the predetermined and locked, operating position.

Abstract: An antenna mounting system for use with recreational vehicles and boats as well as stationary objects. The system includes a pedestal securable to the recreational vehicle and an antenna head containing an antenna element and securable to the pedestal. The pedestal has an upstanding male portion slidably receivable in a mating, female portion of the antenna head. In assembling the system, the male and female portions are first axially aligned and then moved axially toward each other to a predetermined, operating position where they are snapped together in a locking engagement. Anti-rotation structure including one or more pairs of mating, channels and protuberance is also provided to prevent the pedestal and antenna head from being rotated relative to each other about their aligned axes (and the coaxial cable running through them from being twisted) as they are moved together to the predetermined and locked, operating position.

Abstract: An apparatus and method for quickly releasing, without using any tools, the dome from the base of a domed satellite antenna system. An actuator moves in each of a number of quick-release fasteners around the dome to an unlocked position. The dome is lifted to reveal the operational components, the revealed components can then be changed (e.g., by setting switches to receive different satellites), and then the dome is replaced over the base. Each actuator is moved to the locked position to re-attach the dome to the base.