“…Many of these studies have been coupled with preliminary hybrid rocket engine or component design, assessing methods for particle transport and dispersion as well as engine configuration [2,5]. The potential benefits of CO 2 -Mg(s) have also been addressed, being incorporated into various mission concepts [2,3,10,11]. Lastly, the feasibility of CO 2 -Mg(s) has been demonstrated, with both rocket and turbojet engines being built and successfully producing thrust [12,13] for abbreviated periods of time.…”