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Development, Qualification and First Flight Data of the Iodine Based Cold Gas Thruster for CubeSats

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conference contribution
posted on 04.03.2020, 08:41 by Javier Martínez MartínezJavier Martínez Martínez, Dmytro Rafalskyi, Elena Zorzoli Rossi, Ane Aanesland
In this work we describe the development process and present the first flight results obtained for the I2T5, the first ever iodine-based propulsion system launched to space in November 2019. The system uses the sublimation of
solid iodine to build up a gas pressure in the storage tank, which is then guided to the nozzle. The main challenge of using iodine as a propellant in a cold gas
propulsion system is the corrosive nature of the iodine, which is a halogen with moderate chemical activity towards most of the metals including stainless steel, as well as other common substances found in spacecrafts. The acceleration
of flows in such system is also a complex task, since the maximum vapor pressure of the propellant is defined by the maximum allowed temperature of operation, chosen to avoid solid-to-liquid phase transition which would result in the need to use precise micro-nozzles. The other challenges,
such as the possibility of fragmentation of the propellant with consequent loss of the thermal contact and “bouncing” in microgravity conditions, have also been studied and resolved. Here we present the main approaches to our development process and describe the key solutions which resulted in having a space-ready operational device.

Funding

Le Grand Prix I-LAB 2017 - 19th Concours National d’Aide à la Création d’Entreprises de Technologies Innovantes

CNES INODIN grant, R&T action R-S19/PF-0002-108-92

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