We are thrilled to share the key objectives of the iFACT-MP project, which is dedicated to developing an iodine-fed thruster subsystem for the 3-5 kW power range and advancing it to TRL5. Here's what we're working on:
OBJECTIVES
Thruster: Scale up the Advanced Cusp Field Thruster (ACFT) to the 3-5 kW power range to address the demands of higher power class applications.
Cathode: Develop an iodine-fed hollow cathode with C12A7 emitters, achieving enhanced performance characteristics for advanced electric propulsion applications.
Fluidics: Establish a complete chain for the iodine Electric Propulsion (EP) system, including a heated tank, flow control mechanism, and piping.
METHODOLOGY
Test Facility: Create an iodine-compatible vacuum chamber capable of enabling thorough characterization and endurance testing at the required power level.
Diagnostics: Pioneering the development of an optical sensor designed to measure iodine flow rate in-situ, enhancing precision and monitoring capabilities.
IMPACT
Specification: Perform a comprehensive analysis of market and platform requirements to define the key specifications for a competitive and advanced Electric Propulsion (EP) subsystem.
Stay connected for more updates as we push the boundaries of space technology!