Rigorous Antenna Noise Temperature Calculation Method for International Space Station Visiting Spacecraft

摘要

The temperature of the orbiting space station's Sun-facing side could be up to 250 ℉ (≈120 ℃) and will be a significant antenna noise temperature contributor for visiting spacecraft communication and tracking systems during rendezvous. The conventional antenna noise temperature calculation does not take into account the space station reflection effects, and results in an underestimated antenna and system noise temperature. Thus, the visiting spacecraft communication and tracking" system performance could be overestimated during rendezvous.