Thermal Sensitivity Analysis of a Telemetry Antenna in Sub-Orbital Spaceflights

A thermal sensitivity analysis is performed for an Inverted-F antenna (IFA) at the worst-case thermal condition (reentry phase) of a typical sub-orbital sounding-rocket spaceflight. Electromagnetic simulations show that a ۳۰۰ Celsius change in the IFA temperature, mainly caused by the aerodynamic heating, increases the reflected power by ۱% and decreases the antenna gain by ۲.۵%. The results show that the degradation of antenna performance and the telemetry link quality is negligible. Therefore, the IFA is a good antenna choice for similar sounding rockets from the thermal reliability point of view.

Keywords:

antenna , Inverted-F antenna , Thermal sensitivity analysis , Aerodynamic heating , Electromagnetic simulation