Author:
Ide Yuichiro,Takahashi Takuya,Iwai Keiichiro,Nozoe Katsuhiko,Habu Hiroto,Tokudome Shinichiro
Reference10 articles.
1. V. Bombelli, D. Simon, T. Marée, J.L. Moerel, Economic Benefits of the use of Non-Toxic Mono-propellants for Spacecraft Applications, in: 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, Alabama, AIAA-2003-4783.
2. A. Larsson and N. Wingborg, Green Propellants Based on Ammonium Dinitramide (ADN), Advances in Spacecraft Technologies, J. Hall. (Ed.), ISBN: 978-953-307-551-8, InTech. Rijeka, 2011.
3. J. S. Wilkes, A short history of ionic liquids—from molten salts to neoteric solvents, Green Chem., 4 (2002) 73-80.
4. T. Katsumi, H. Kodama, T. Matsuo, H. Ogawa, N. Tsuboi, K. Hori, Combustion Characteristics of a Hydroxylammonium Nitrate Based Liquid Propellant. Combustion Mechanism and Application to Thrusters, Combustion, Explosion, and Shock Waves, Vol. 45, No. 4 (2009) 442-453.
5. H. J. Liaw, C.C. Chen, Y.C. Chen, J.R. Chen, S.K. Huang, S.N. Liu, Relationship between Flash Point of Ionic Liquids and their Thermal Decompositin, Creen Chem., 14 (2012) 2001-2008.
Cited by
35 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献