In this paper, architectures for interplanetary communications that feature the use of a data relay are investigated. In the considered "two-leg" architecture, a spacecraft orbiting the Earth, or in orbit at a Lagrange point, receives data from a deep space probe (leg-1) and relays them towards ground (leg-2). Different wireless technologies for the interplanetary link, namely, radio frequencies above the Ka band and optical frequencies, are considered. Moreover, the cases of transparent and regenerative relaying as well as different different orbital configurations are addressed, offering a thorough analysis of such systems from different viewpoints. Results show that, under certain constraints in terms of pointing accuracy and onboard antenna size, the adoption of a two-leg architecture can achieve the data rates supported by direct space-to-Earth link configurations with remarkably smaller ground station antennas.
I. INTRODUCTIONT HE use of extremely high radio frequency (RF) bands or optical frequencies in wireless digital communication systems is known to potentially allow achieving very high data rates, compared with the ones achievable at lower frequencies, for the same error rate performance. Such extremely high frequency bands are, however, seldom employed in deep space communication links due to their vulnerability to atmospheric impairments. They may, nevertheless, provide several advantages in deep space telemetry (TM) and telecommand (TC) links in the framework of a "two-leg" relay architecture. Accordingly, a spacecraft (S/C) orbiting the Earth or in orbit at a Lagrange point would receive TM data from a deep space probe and would relay them to the ground station (G/S). The deep space to relay link, not affected by the Earth atmosphere, may take advantage of an extremely high frequency band, e.g., frequencies between Ka-band ones and 75 GHz (which include the Q/V band), or the optical band, while the second link