Phased arrays of reflector antennas can be used to obtain effective area and gain that are much larger than is practical with a single antenna. This technique is routinely used by NASA for receiving weak signals from deep space. Phase alignment of the signals can be disrupted by turbulence in the troposphere, which causes fluctuations in the differences of signal delays among the antennas. At the Deep Space Network stations, site test interferometers (STIs) are being used for long-term monitoring of these delay fluctuations using signals from geostationary satellites. In this paper, we compare the STI measurements with the phase variations seen by a nearby two-element array of 34 m diameter antennas tracking 8.4 GHz and 32 GHz signals from the Cassini spacecraft in orbit around Saturn. It is shown that the statistics of the STI delay fluctuations, after appropriate scaling for differences in antenna separation and elevation angle and conversion to phase at the spacecraft frequencies, provide reliable estimates of the phase fluctuations seen by the large antennas on the deep space signal. Techniques for adaptive compensation of the phase fluctuations are available when receiving a sufficiently strong signal, but compensation is often impractical or impossible when using the array for transmitting. These results help to validate the use of long-term STI data for assessing the feasibility of large transmitting arrays at various sites. This paper will discuss the results of array demonstration tracks using 34 m diameter antennas located at Goldstone, California, which received signals emitted by the Cassini spacecraft [Kliore et al., 2004]. The Cassini spacecraft's 32 GHz downlink carrier was turned on for radio science experiments or engineering demonstrations involving a single 34 m antenna. A second antenna was allocated in each case for the purpose of conducting twoelement arraying demonstrations. We present and discuss results from the array demonstrations involving two 34 m diameter antennas at Goldstone designated as DSS-25 and DSS-26. The Cassini array demonstrations were MORABITO ET AL. ARRAY/INTERFEROMETER INTERCOMPARISON 91 PUBLICATIONS