1. 1) Nakagawa, T., Mihara, Y. and Komurasaki, K.: Propulsive Impulse Measurement of a Microwave-Boosted Vehicle in the Atmosphere, J. Space. Rockets, 41 (2004), pp. 151–153.
2. 2) Oda, Y., Komurasaki, K., Takahashi, K., Kasugai, A., and Sakamoto, K.: Plasma Generation Using High-Power Millimeter-Wave Beam and Its Application for Thrust Generation, J. Appl. Phys., 100 (2006),113307.
3. 3) Oda, Y.: Application of Atmospheric Millimeter Wave Plasma to Rocket Propulsion, Doctor Thesis, The University of Tokyo (2008).
4. 4) Fukunari, M., Komatsu, R., Arnault, A., Yamaguchi, T., Komurasaki, K., and Arakawa, Y.: Air-Breathing Performance of Microwave Rocket with Reed Valve System, Vacuum, 88 (2013), pp. 155–159.
5. 5) Fukunari, M., Arnault, A., Yamaguchi, T., and Komurasaki, K.: Replacement of Chemical Rocket Launchers by Beamed Energy Propul sion, Appl. Optics, 53 (2014), pp. 16–22.