Abstract
Liquefied hydrogen peroxide has attracted attention as a mono-propellant energy source for systems that require a simple, lightweight structure. Its application has been extended to aerospace and deep-sea submarine systems, because this system has no need of an oxidizer and no hazardous products are discharged. For further industrial applications, however, a feasibility study should be carefully conducted with respect to power-supply efficiencies such as specific power density. In the present study, a prototype of a vane motor driven by liquefied hydrogen peroxide with a high density (95%) was developed and performance characteristics such as the specific power density were estimated by measuring the pressure and rotation speed of the vane motor, and by numerical simulation using FSI (Fluid-Structure-Interaction) analysis. The obtained specific power density reached 0.02 kW/kgf, which approximates the levels of the most up-to-date fuel cells.
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Lee, H., Kim, W., Han, J., and Han, C., “The Technical Trend of the Exoskeleton Robot System for Human Power Assistance,” Int. J. Precis. Eng. Manuf., Vol. 13, No. 8, pp. 1491–1497, 2012.
Kazerooni, H., “Exoskeletons for Human Power Augmentation,” Proc. of IEEE/RSJ International Conference on intelligent Robots and Systems, pp. 3120–3125, 2005.
Shields, B. and Goldfarb, M., “Design and Energetic Characterization of a Solenoid Injected Liquid Monopropellant Powered Actuator for Self-Powered Robots,” Proc. of IEEE International Conference on Robotics and Automation, pp. 241–246, 2005.
Ha, S. U., Kwon, M. C., Seo, K. S., and Han, S. Y., “The Past and Future Perspective of Hydrogen Peroxide as Rocket Propellants,” The Korean Society for Aeronautical & Space Sciences, Vol. 37, No. 7, pp. 717–728, 2009.
Jin, J. K. and Kwon, S. J., “Catalytic combustion of H2/Air mixture using Pt/Al2O3 coated nickel foam,” KOSCO SYMPOSIUM, pp. 37–44, 2007.
An, S. Y., Park, D. J., Chung, S. M., and Kwon, S. J., “The Response Characteristics of the Hydrogen Peroxide Monopropellant Thruster as Injector and Catalyst Grain Size,” The Korean Society of Propulsion Engineers, Vol. 13, No. 1, pp. 19–26, 2009.
Lee, D. H. and Kwon, S. J., “Development of Analysis Model for Down Scaled Two Phase Catalytic Reactor,” Trans. Korean Soc. Mech. Eng. B, Vol. 28, No. 1, pp. 24–30, 2004.
Lee, S. T. and Lee, J. B., “Technology of N2H4 Mono-propellant Thruster for the Satellite Attitude Control,” KSME SYMPOSIUM, pp. 43–52, 2002.
Cho, C. H., Lee, D. H., and Kwon, S. J., “Experimental Study on Millimeter Scale Two Phase Catalytic Reactor,” Trans. Korean Soc. Mech. Eng. B, Vol. 28, No. 3, pp. 265–270, 2004.
Jansen, J. F., Richardson, B., Pin, F., Lind, R., and Birdwell, J., “Exoskeleton for Soldier Enhancement Systems Feasibility Study,” Energy Citations Database, 2000.
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Hong, DE., Ryu, GR., Lee, KH. et al. Performance evaluation of a vane motor driven by liquefied hydrogen peroxide. Int. J. Precis. Eng. Manuf. 14, 1163–1167 (2013). https://doi.org/10.1007/s12541-013-0158-z
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DOI: https://doi.org/10.1007/s12541-013-0158-z