Pure and Applied Chemistry

CrossRef Cited-by Linking

• Naya Tomoki, Kohga Makoto: Influences of particle size and content of RDX on burning characteristics of RDX-based propellant. Aerospace Science and Technology 2014, 32, 26. <http://dx.doi.org/10.1016/j.ast.2013.12.004>
• McDonald Brian A., Rice Jeremy R., Kirkham Mark W.: Humidity induced burning rate degradation of an iron oxide catalyzed ammonium perchlorate/HTPB composite propellant. Combustion and Flame 2014, 161, 363. <http://dx.doi.org/10.1016/j.combustflame.2013.08.014>
• Naya Tomoki, Kohga Makoto: Influences of particle size and content of HMX on burning characteristics of HMX-based propellant. Aerospace Science and Technology 2013, 27, 209. <http://dx.doi.org/10.1016/j.ast.2012.08.012>
• Maggi Filippo, Gariani Gabriela, Galfetti Luciano, DeLuca Luigi T.: Theoretical analysis of hydrides in solid and hybrid rocket propulsion. International Journal of Hydrogen Energy 2012, 37, 1760. <http://dx.doi.org/10.1016/j.ijhydene.2011.10.018>
• Muravyev Nikita, Frolov Yurii, Pivkina Alla, Monogarov Konstantin, Ordzhonikidze Olga, Bushmarinov Ivan, Korlyukov Alexander: Influence of Particle Size and Mixing Technology on Combustion of HMX/Al Compositions. Propellants Explos Pyrotech 2010, 35, 226. <http://dx.doi.org/10.1002/prep.201000028>
• Monogarov K. A., Meerov D. B., Ivanov D. A., Ordzhonikidze O. S., Frolov Yu. V., Pivkina A. N., Korlyukov A. A., Bushmarinov I. S., Muravyov N. V.: Structural and functional diagnostics of ultrafine components in condensed high-energy systems. J Struct Chem 2010, 51, 109. <http://dx.doi.org/10.1007/s10947-010-0198-5>
• Kohga Makoto: Burning Rate Characteristics of Ammonium Perchloarte-Based Composite Propellant Using Bimodal Ammonium Perchlorate. Journal of Propulsion and Power 2008, 24, 499. <http://dx.doi.org/10.2514/1.27107>
• Felix S. Prem, Singh Gurdip, Sikder A.K., Aggrawal J.P.: Studies on energetic compounds. Thermochimica 2005, 426, 53. <http://dx.doi.org/10.1016/j.tca.2004.06.020>
• Massa L., Jackson T. L., Buckmaster J.: New Kinetics for a Model of Heterogeneous Propellant Combustion. Journal of Propulsion and Power 2005, 21, 914. <http://dx.doi.org/10.2514/1.2433>
• Singh Gurdip, Prem Felix S, Soni Pramod: Studies on energetic compounds part 28: thermolysis of HMX and its plastic bonded explosives containing Estane. Thermochimica 2003, 399, 153. <http://dx.doi.org/10.1016/S0040-6031(02)00460-4>
• Shusser Michael, C. Culick Fred E., Cohen Norman S.: Combustion Response of Ammonium Perchlorate Composite Propellants. Journal of Propulsion and Power 2002, 18, 1093. <http://dx.doi.org/10.2514/2.6039>
• Al-Harthi A., Williams A.: Effect of fuel binder and oxidiser particle diameter on the combustion of ammonium perchlorate based propellants. Fuel 1998, 77, 1451. <http://dx.doi.org/10.1016/S0016-2361(98)00059-3>
• BILGER R. W., JIA X., Ll J. D., NGUYEN T. T.: Theoretical and Experimental Study of Composite Solid Propellant Combustion. Combust Sci Techn 1996, 115, 1. <http://dx.doi.org/10.1080/00102209608935521>