Preliminary Development of a Hydrogen Peroxide Thruster
Green propellants used for satellite-level propulsion system become attractive in recent years because the non-toxicity and lower requirements of safety protection. One of the green propellants, high-concentration hydrogen peroxide H2O2 solution (≥70% w/w, weight concentration percentage), often known as high-test peroxide (HTP), is considered because it is ITAR-free, easy to manufacture and the operating temperature is lower than traditional monopropellant propulsion. To establish satellite propulsion technology, the National Space Organization (NSPO) in Taiwan has initialized a long-term cooperation project with the National Cheng Kung University to develop compatible tank and thruster. An experimental propulsion payload has been allocated for the future self-reliant satellite to perform orbit transfer and maintenance operations. In the present research, an 1-Newton thruster prototype is designed and the thrusting force is measured by a pendulum-type platform. The preliminary hot-firing test at ambient environment showed the generated thrust and the specific impulse are about 0.7 Newton and 102 seconds, respectively.
Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1087287Procedia APA BibTeX Chicago EndNote Harvard JSON MLA RIS XML ISO 690 PDF
 W. J. Larson and J. R. Wertz, Space Mission Analysis and Design, Second Edition, Microcosm, Inc., 1992.
 G. P. Sutton, Rocket Propulsion Elements, John Wiley & Sons, Inc., 1992.
 R. W. Humble, G. N. Henry, and W. J. Larson, Space Propulsion Analysis and Design, The McGraw-Hill Companies, Inc., Primis Custom Publishing, 1995.
 M. Tajmar, Advanced Space Propulsion Systems, Springer, 2003.
 W. C. Schumb, C. N. Satterfield, and R. L. Wentworth, Hydrogen Peroxide, Reinhold Publishing Company, New York, 1955.
 D. Andrews, “The Industrial History of the Ansty Rocket Department, 1946 to 1971,” July 26, 1998
 L. E. James and W. H. Stillwell, “The Hydrogen-Peroxide Rocket Reaction-Control System for the X-1B Research Airplane,” NASA Technical Note TN D-158, Flight Research Center, Edwards, CA, Dec. 1959.
 J. F. Runckel, C. M. Willis, L. B. Salters Jr., “Investigation of Catalyst Beds for 98-Percent-Concentration Hydrogen Peroxide,” NASA TN D-1808, Langley Research Center, Hampton, Virginia, 1963.
 W. E. Armstrong, C. Z. Morgan, L. B. Ryland, and H. H. Voge, "Development of Catalysts for Monopropellant Hydrazine Decomposition,'' Shell Development Company Report No. S-13947, Contract NAS 7-97, 1964.
 J. Clark, Ignition - An Informal History of Liquid Rocket Propellants, Rutgers University Press, New Brunswick, 1972.
 E. Wernimont and P. Mullens, “Recent Developments in Hydrogen Peroxide Monopropellant Devices,” AIAA-99-2741, General Kinetics, LLC, Aliso Viejo, CA
 D. L. Hitt, C. M. Zakrzwski, and M. A. Thomas, "MEMS-based satellite micropropulsion via catalyzed hydrogen peroxide decomposition, Smart Mater. Struct., vol. 10, pp. 1163–1175, 2001.
 J. Ponzo, “Small Envelope, High Flux 90% Hydrogen Peroxide Catalyst Bed,” 39th AIAA/ASME/SAE/ASE Joint Propulsion Conference and Exhibit, Huntsville, Alabama, 20-23 July 2003,
 C. Scharlemann, M. Schiebl, R. Amsüss, and M. Tajmar, “Development of Miniaturized Green Propellant Based Mono- and Bipropellant Thrusters,” 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA 2007-5580, Cincinnati, OH, 8 - 11 July 2007.
 A. Pasini, L. Torre, L. Romeo, A. Cervone, L. d’Agostino, A. J. Musker, and G. Saccoccia, “Experimental Characterization of a 5 N Hydrogen Peroxide Monopropellant Thruster Prototype,” 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA-2007-5465, Cincinnati, OH, 8 - 11 July 2007
 S. L. Lee and C. W. Lee, “Performance characteristics of silver catalyst bed for hydrogen peroxide,” Aerospace Science and Technology, vol. 13, no. 1, pp. 12–17, 2009.
 L. Pirault-Roy, C. Kappenstein, M. Guèrin, R. Eloirdi, and N. Pillet, “Hydrogen Peroxide Decomposition on Various Supported Catalysts Effect of Stabilizers,” Journal of Propulsion and Power, vol. 18, no. 6, 2002, pp. 1235–1241.
 Y. A. Chan, H. W. Hsu, and Y. C. Chao, “Development of a HTP Mono-propellant Thruster by Using Composite Silver Catalyst,” 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, San Deigo, CA, 31 July - 3 August, 2011.