Performance Assessment of 1 N Bipropellant Thruster Using Green Propellants H2O2/Kerosene
2012; American Institute of Aeronautics and Astronautics; Volume: 29; Issue: 1 Linguagem: Inglês
10.2514/1.b34633
ISSN1533-3876
AutoresDavid Krejci, A. Woschnak, Carsten Scharlemann, Karl Ponweiser,
Tópico(s)Energetic Materials and Combustion
ResumoNo AccessTechnical NotePerformance Assessment of 1 N Bipropellant Thruster Using Green Propellants H2O2/KeroseneDavid Krejci, Alexander Woschnak, Carsten Scharlemann and Karl PonweiserDavid KrejciAerospace Engineering, FOTEC GmbH, 2700 Wiener Neustadt, Austria, Alexander WoschnakAerospace Engineering, FOTEC GmbH, 2700 Wiener Neustadt, Austria, Carsten ScharlemannAerospace Engineering, University of Applied Sciences Wiener Neustadt, 2700 Wiener Neustadt, Austria and Karl PonweiserInstitute for Energy Systems and Thermodynamics, Vienna University of Technology, 1040 Vienna, AustriaPublished Online:28 Jan 2013https://doi.org/10.2514/1.B34633SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Ponzo J., "Small Envelope, High Flux 90% Hydrogen Peroxide Catalyst Bed," 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 2003-4622, 2003. LinkGoogle Scholar[2] Ventura M., Wernimont E., Heister S. and Yuan S., "Rocket Grade Hydrogen Peroxide (RGHP) for use in Propulsion and Power Devices: Historical Discussion of Hazards," 43th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 2007-5468, 2007. LinkGoogle Scholar[3] "Hydrogen Peroxide Handbook," Chemical and Material Science Dept./Rocketdyne, Technical Rept. No. AFRPL-TR-67-144, 1967. Google Scholar[4] Wiswell R. L., "X-15 Propulsion System," 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 1997-2682, 1997. LinkGoogle Scholar[5] McCormick J., Hydrogen Peroxide Rocket Manual, FMC Corp., Buffalo, N.Y., 1967. Google Scholar[6] Scharlemann C., "Green Propellants: Global Assessment of Suitability and Applicability," European Conference for Aerospace Sciences (EUCASS), Versailles, France, 2000. Google Scholar[7] Scharlemann C., "Experimental Verification of Green Propellant Candidates: An Overview of GRASP Activities," 4th European Conference for Aerospace Sciences (EUCASS), Saint Petersburg, Russia, 2011. Google Scholar[8] Whitehead J. C., "Hydrogen Peroxide Propulsion for Smaller Satellites," 12th Annual AIAA/USU Conference on Small Satellites, AIAA Paper 2006-5239, 2006. Google Scholar[9] Rusek J. J., "Hydrogen Peroxide for Propulsion and Power Applications: A Swift Perspective," Proceedings of the 2nd International Conference on Green Propellants for Space Propulsion, AIAA Paper 2009-4842, 2009. Google Scholar[10] Scharlemann C., "Green Propellants: Global Assessment of Suitability and Applicability," European Conference for Aerospace Sciences (EUCASS), Versailles, France, 2009. Google Scholar[11] Sahara H., Nakasuka S., Sugawara Y. and Kobayashi C., "Demonstration of Propulsion System for Microsatellite Based on Hydrogen Peroxide in SOHLA-2 Project," 43th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 2007-5575, 2007. LinkGoogle Scholar[12] Wernimont E. J., "Monopropellant Hydrogen Peroxide Rocket Systems: Optimum for Small Scale," 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 2006-4549, 2006. LinkGoogle Scholar[13] Whitehead J. C., Dittman M. D. and Ledebuhr A. G., "Progress Toward Hydrogen Peroxide Micropropulsion," 13th Annual AIAA/USU Conference on Small Satellites, Utah State Univ. Paper SSC99-XII-5, 1999. Google Scholar[14] Scharlemann C., "Experimental Verification of Green Propellant Candidates: An Overview of GRASP activities," 4th European Conference for Aerospace Sciences (EUCASS), Saint Petersburg, Russia, 2011. Google Scholar[15] Barley S., Palmer P. L. and Coxhill I., "Evaluating the Miniaturisation of a Monopropellant Thruster," 42nd AIAA/ASMA/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA Paper 2006-4549, 2006. LinkGoogle Scholar[16] Torre L., Pasini A., Romeo L. and d'Agostino L., "Firing Performance of Advanced Hydrogen Peroxide Catalytic Beds in a Monopropellant Thruster Prototype," 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 2008-4937, 2008. LinkGoogle Scholar[17] Pasini A., Torre L., Romeo L., Cervone A. and d'Agostino L., "Endurance Tests on Different Catalytic Beds for H2O2 Monopropellant Thrusters," 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 2009-5472. Google Scholar[18] Sungyong A. and Kwon S., "Catalyst Bed Sizing of 50 Newton Hydrogen Peroxide Monopropellant Thruster," 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 2008-5108, 2008. Google Scholar[19] An S., Jo S., Wee J., Yoon H. and Kwon S., "Preliminary Flight Test of Hydrogen Peroxide Retro-Propulsion Module, Acta Astronautica, Vol. 67, Nos. 5–6, 2010, pp. 605–612. doi:https://doi.org/10.1016/j.actaastro.2010.04.010 AASTCF 0094-5765 CrossrefGoogle Scholar[20] Whitehead J. C., Dittman M. D. and Ledebuhr A. G., "Progress Toward Hydrogen Peroxide Micropropulsion," 13th Annual AIAA/USU Conference on Small Satellites, Utah State Univ. Paper No. SSC99-XII-5, Aug. 1999. Google Scholar[21] Woschnak A., Krejci D., Schiebl M. and Scharlemann C., "Development of a Green Bipropellant Hydrogen Peroxide Thruster for Attitude Control on Satellites," 4th European Conference for Aerospace Sciences (EUCASS), Saint Petersburg, Russia, 2011. Google Scholar[22] Haag G. S., Sweeting M. N. and Richardson G., "Low Cost Propulsion Development for Small Satellites at the Surrey Space Centre," 13th Annual AIAA/USU Conference on Small Satellites, Utah State Univ. Paper No. SSC99-XH-2, Aug. 1999. Google Scholar[23] Barley S., Palmer P. L. and Coxhill I., "Evaluating the Miniaturization of a Monopropellant Thruster," 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 2006-4549, 2006. LinkGoogle Scholar[24] Bramanti C., Cervone A., Romeo L., Torre L., d'Agostino L., Musker A. J. and Saccoccia G., "Experimental Characterization of Advanced Materials for the Catalytic Decomposition of Hydrogen Peroxide," 42th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 2006-5238, Sacramento, CA. Google Scholar[25] Kappenstein C., Pirault–Roy L., Guerin M., Wahdan T., Ali A. A., Al-Sagheer F. A. and Zaki M. I., "Monopropellant Decomposition Catalysts: V. Thermal Decomposition and Reduction of Permanganates as Models for the Preparation of Supported MnOx Catalysts," Applied Catalysis A: General, Vol. 234, No. 1, 2002, pp. 145–153.doi:https://doi.org/10.1016/S0926-860X(02)00220-X ACAGE4 0926-860X CrossrefGoogle Scholar[26] Richardson J. T., Remue D. and Hung J.-K., "Properties of Ceramic Foam Catalyst Supports: Mass and Heat Transfer," Applied Catalysis A: General, Vol. 250, No. 2, 2003, pp. 319–329.doi:https://doi.org/10.1016/S0926-860X(03)00287-4 ACAGE4 0926-860X CrossrefGoogle Scholar[27] Torre L., Pasini A., Romeo L. and d'Agostino L., "Firing Performance of Advanced Hydrogen Peroxide Catalytic Beds in a Monopropellant Thruster Prototype," 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA Paper 2008-4937, 2008. LinkGoogle Scholar[28] Lee S.-L. and Lee C.-W., "Performance Characteristics of Silver Catalyst Bed for Hydrogen Peroxide," Aerospace Science and Technology, Vol. 13, No. 1, 2009, pp. 12–17.doi:https://doi.org/10.1016/j.ast.2008.02.007 ARSTFZ 1270-9638 CrossrefGoogle Scholar[29] Musker A. J., "Development of a 200 Newton Bipropellant Thruster Using Heterogeneous Catalytic Reduction of Hydrogen Peroxide," 4th European Conference for Aerospace Sciences (EUCASS), Saint Petersburg, Russia, 2011. Google Scholar[30] Blank R. A., Pourpoint T. L. and Meyer S. E., "Experimental Study of Flow Processes and Performance of a High Pressure Hydrogen Peroxide Catalyst Bed," 43rd AIAA/ASMA/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA Paper 2007-5469, 2007. LinkGoogle Scholar[31] Lim H., An S., Kwon S. and Rang S., "Hydrogen Peroxide Gas Generator with Dual Catalytic Beds for Nonpreheating Startup," Journal of Propulsion and Power, Vol. 23, No. 4, 2007, pp. 1147–1150.doi:https://doi.org/10.2514/1.28897 JPPOEL 0748-4658 LinkGoogle Scholar[32] Hitt D. L., Zakrazwski C. M. and Thomas M. A., "MEMS-Based Satellite Micropropulsion via Catalyzed Hydrogen Peroxide Decomposition," Smart Materials and Structures, Vol. 10, No. 6, 2001, pp. 1163–1175. doi:https://doi.org/10.1088/0964-1726/10/6/305 SMSTER 0964-1726 CrossrefGoogle Scholar[33] Cen J. W. and Xu J. L., "Performance Evaluation and Flow Visualization of a MEMS Based Vaporization Liquid Micro-Thruster, Acta Astronautica, Vol. 67, Nos. 3–4, 2010, pp. 468–482.doi:https://doi.org/10.1016/j.actaastro.2010.04.009 AASTCF 0094-5765 CrossrefGoogle Scholar[34] Sadov V., "HP-Based Green Rocket Propellants, International Conference on Green Propellants for Space Propulsion," ESA, Noordwijk, Netherlands, 2001. Google Scholar[35] Sisco J. C., Austin B. L., Mok J. S. and Anderson W. E., "Autoignition of Kerosene by Decomposed Hydrogen Peroxide in a Dump-Combustor Configuration," Journal of Propulsion and Power, Vol. 21, No. 3, 2005, pp. 450–459. doi:https://doi.org/10.2514/1.5287 JPPOEL 0748-4658 LinkGoogle Scholar[36] Campolo M., Andreoli M. and Soldati A., "Computing Flow, Combustion, Heat Transfer and Thrust in a Micro-Rocket via Hierarchical Problem Decomposition," Microfluidics and Nanofluidics, Vol. 7, No. 1, 2009, pp. 57–73.doi:https://doi.org/10.1007/s10404-008-0362-9 MNIAAR 1613-4982 CrossrefGoogle Scholar[37] Sadov V., "HP-Based Green Rocket Propellants," International Conference on Green Propellants for Space Propulsion," ESA, Noordwijk, Netherlands, 2001. Google Scholar[38] Sisco J. C., "Autoignition of Kerosene by Decomposed Hydrogen Peroxide in a Dump Combustor Configuration," Master Thesis, Purdue Univ., West Lafayette, IN, 2003. Google Scholar[39] Schiebel M., Krejci D., Woschnak A., Winter F., Lang M. and Scharlemann C., "Modeling and Experimental Verification of Auto-Ignition Processes for a Green Bipropellant Thruster," 61st International Astronautical Congress, International Astronautical Federation, CZ, 2010. Google Scholar[40] Chigier N. A. and Beér J. M., "Velocity and Static-Pressure Distributions in Swirling Air Jets Issuing from Annular and Divergent Nozzles," Journal of Basic Engineering, Vol. 68, No. 4, 1964, pp. 788–797. JBAEAI 0021-9223 CrossrefGoogle Scholar[41] Elliott D. G., Bartz D. R. and Silver S., "Calculation of Turbulent Boundary-Layer Growth and Heat Transfer in Axi-Symmetric Nozzles," Jet Propulsion Lab., Technical Rept. 32-387, 1963. Google Scholar[42] Gordon S. and McBride B. J., "Computer Program for Calculation of Complex Chemical Equilibrium Compositions, Rocket Performance, Incident and Reflected Shocks and Chapman—Jouget detonations," NASA SP-273, 1976. Google Scholar[43] Muss J. A., Johnson C. W., Kruse W. and Cohn R. K., "The Performance of Hydrocarbon Fuels with H2O2 in a Uni-element Combustor," 39th AIAA/ASMA/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA Paper 2003-4623, 2003. LinkGoogle Scholar Previous article
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