In the early 1960s, a new large-aperture, low-noise Advanced Antenna System was in its planning and early development stages for the Deep Space Instrumentation Facility (later known as the Deep Space Network). Compared with the 85-ft (26-meter) antennas then in use, the new antenna was to give a 10-decibel performance increase, with an order of magnitude increase in the data rate from future spacecraft. Feasibility studies and testing were conducted by NASA's Jet Propulsion Laboratory in Pasadena, California, and subcontractors for various technologies and antenna components.
This January 1962 photo shows a 960-mc one-tenth scale Cassegrain antenna feed system study for the Advanced Antenna System. The objective was to establish the electrical performance capabilities and operational feasibility of this type of feed system for large antennas. The mount of the test system was covered with epoxy fiberglass and polystyrene foam to limit reflection of energy during testing.
A 210-foot (64-meter) antenna, using the new technology and designs, was built at the Goldstone site in California and became operational in 1966. The antenna, DSS 14, became known as the Mars antenna when it was used to track the Mariner 4 spacecraft. It was later upgraded to 70 meters in order to track Voyager 2 as it reached Neptune.