Abstract
The study is to perform dynamic link analysis to determine the earliest separation time of the Space Vehicle (SV) from the Launch Vehicle (LV) while meeting the SV link requirements for Telemetry, Tracking and Control (TT&C) uplink & downlink services from/to ground stations. Successful rocket launch required adequate link coverage throughout the flight and good Radio Frequency (RF) performance. The presentation will discuss the concept of the dynamic link analysis, SV antenna switching schedule, recommended SV separation time, as well as the performance for different launch scenarios within the 24-hour launch window. Topics will include antenna patterns, launch trajectories, elevation angle, and clock & cone angle geometry, and dynamic link budget.
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