1. 1) Kawaguchi, J., Morita, Y., Nakajima, T., Ishii, N., Hashimoto, T., Yamakawa, H., Hirokawa, E., Yasuda, S. and Balloon Group: Flight Test of the Rhumb Line Control System via Balloon, Proceedings of the 3rd Workshop on Astrodynamics and Flight Mechanics, 1993, pp.156-161.
2. 2) Kawaguchi, J.: On the Simplified Recursive Formula of Rhumb Line Maneuvers with its Application to Identification of Directional Dispersion, Proceedings of the 3rd Workshop on Astrodynamics and Flight Mechanics, 1993, pp.194-199.
3. 3) Yamamoto, T., Mori, O., Shida, M. and Kawaguchi, J.: Development of Gas-Liquid Equilibrium Thruster for Small Satellite, International Symposium on Space Technology and Science, ISTS 2006-k-32, 2006.
4. 4) Tsuda, Y., Mori, O., Nishimura. Y. and Kawaguchi,J.: Deployment Experiment of Thin Flexible Membrane Using Sounding Rocket for Future Solar Sail Mission, International Symposium on Space Technology and Science, ISTS 2004-c-11, 2004.
5. 5) Nishimura, Y., Tsuda, Y., Mori, O. and Kawaguchi, J.: The Deployment Experiment of Solar Sail with Sounding Rocket, 55th International Astronautical Congress, IAC-04-A.5.10, 2004.