1. “You can get there from here”: advanced low cost propulsion concepts for small satellites beyond LEO;Baker;Acta Astronaut,2005
2. Bonafacio S. Analysis and design of a multi-phase catalytic reactor for the decomposition of hydrogen peroxide in space propulsive systems. PhD dissertation, Universita degli Studi di Napoli “Federico II”, Web; 2006.
3. Wernimont E. System trade parameter comparison of monopropellants: hydrogen peroxide vs. hydrazine and others. In: 42 AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit; July 9–12, 2006.
4. http://femci.gsfc.nasa.gov/workshop/2003/presentations/varia/Varia-MEMS_Thruster.ppt.