BIT-3 CubeSat System

Busek’s BIT-3 RF ion thruster is a mission enabling, iodine-fueled ion propulsion system scheduled for launch on two deep-space
CubeSat missions aboard NASA’s Space Launch System rocket in 2021. The 56-75 W input propulsion system utilizes a 2.5 cm diameter grid RF ion thruster (BIT-3) and a micro RF cathode (BRFC1) as the neutralizer.

The thruster’s unprecedented performance produces thrust up to 1.1 mN and specific impulse up to 2,150 seconds. Performance results were verified with xenon and iodine propellant using a highly accurate torsional thrust stand. As an optional add-on, Busek has developed an innovative thruster gimbal capable of desaturating reaction wheels as part of the Attitude Control System (ACS).

The BIT-3 uses an inductively-coupled plasma (ICP) discharge to eliminate the need for an internal hot cathode and increase overall lifetime.

The most unique feature of BIT-3 is its compatibility with iodine propellant, a demonstrated drop-in replacement for xenon in terms of thrust and Isp performance. Iodine stores as a dense solid (>2x storage density than xenon) and eliminates the need for high-pressure tanks.

Advances in the BIT-3 thruster and BRFC-1 neutralizer are complemented by major breakthroughs in the flight electronics. The BIT-3 power processing unit (PPU) features a ~90% efficient RF power supply with radiation-tolerant components. The state-of-the-art electronics package is highly efficient and compact.