This thesis investigates the preliminary feasibility study of a new class of ultra-light inflatable antennas with a large transmitting and receiving surface composed of metallized fabric. These antennas are designed for deployment in Low Earth Orbit (LEO), at approximately 2000 km altitude from sea level. The orientation is controlled through the interaction between the Earth’s magnetic field and electric currents induced within conductive elements embedded in the antenna’s structure. This innovative control method eliminates the need for traditional mechanical actuators or booms, reducing complexity, mass, and transportation cost to space, while increasing operational efficiency. A critical challenge associated with inflatable antennas is deployment and ensuring structural integrity of the membrane.