TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
Online ISSN : 1884-0485
ISSN-L : 1884-0485
b) Electric and Advanced Propulsion
Exotic Propellant for Continuous Wave Laser Propulsion
Keisuke KONDOHideyuki HORISAWA
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2014 年 12 巻 ists29 号 p. Tb_47-Tb_50

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In this study, an investigation of an exotic mixture of non-hazardous materials was conducted both in the solid and liquid states, which produced higher heat releases through chemical reactions augmented by low-power continuous wave lasers. Numerical evaluation of exothermic energies, or heat release, through chemical reactions of the target propellants was conducted with a chemical equilibrium calculation code. The results showed that the reaction temperature for B-mixed PTFE was 500 K higher than raw PTFE. In liquid propellants, the highest reaction temperature of over 2000 K was obtained for HFE at low specific energy of 3 kJ/g.
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© 2014 The Japan Society for Aeronautical and Space Sciences
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