참고문헌
- Hass, N. E., Smart, M. K. and Paull, A., "Flight Data Analysis of HyShot 2", 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Coference, AIAA, Capua, Italy, 2005.
- Gardner, A., Hannemann, K., Steelant, J. and Paull, A., "Ground Testing of the Hyshot Supersonic Combustion Experiment in HEG and Comparison with Flight Data", 40th AIAA Joint Propulsion Conference, AIAA, Florida, USA, 2004.
- Paiva, K. V., Mantelli, M. B. H. and Slongo, L. K., "Experimental Testing of Mini Heat Pipes Under Microgravity Conditions Aboard a Suborbital Rocket", Aerospace Science and Technology, Vol. 45, 2015, pp. 367-375. doi: 10.1016/j. ast.2015.06.004
- Stamminger, A., "Re-Entry Analysis of Research Rocket Payloads", 62nd International Astronautical Congress, The International Astronautical Federation, Cape town, South Africa, 2010.
- Lingard, J. S., Saunders, A., Merrifield, J., Caldwell, J., Longo, J. and Ferracina, L., "Supersonic Parachute Testing Using a MAXUS Sounding Rocket Piggyback Payload", 8th European Symposium on Aerothermodynamics for Space Vehicles Proceedings, European Space Agency, Lisbon, Portugal, 2015.
- Stamminger, A., Altenbuchner, L., Ettl, J., Eggers, M. H., Jung, W. and Turner, P., "DLR's Mobile Rocket Base - Flight Tickets for your Microgravity Experiments", 64th International Astronautical Congress, The International Astronautical Federation, Beijing, China, 2013.
- Florin, G., Lockowandt, C. and Abrahamsson, M., "Sounding Rockets and Stratospheric Balloons, Unique Test Paltforms for Re-entry Systems at ESRANGE", 8th European Symposium on Aerothermodynamics for Space Vehicles Proceedings, European Space Agency, Lisbon, Portugal, 2015.
- Savino, R., Aurigemma, R., Aversana, P. D., Gramiccia, L., Longo, J., Marraffa, L., Punzo, F. and Scolamiero, L., "European Sounding Rocket Experiment on Hypersonic Deployable Re-Entry Demonstrator", 8th European Symposium on Aerothermodynamics for Space Vehicles Proceedings, European Space Agency, Lisbon, Portugal, 2015.
- Nagata, H., Ito, M., Maeda, T., Watanabe, M., Uematsu, T., Totani, T. and Kudo, I., "Development of CAMUI Hybrid Rocket to Creat a Market for Small Rocket Experiments", Acta Astronautica, Vol. 59, No. 1-5, 2006, pp. 253-258. doi: 10.1016/j.actaastro.2006.02.031
- Tsohas, J., Appel, B., Rettenmaier, A., Walker, M. and Heister, S. D., "Development and Launch of the Purdue Hybrid Rocket Technology Demonstrator", 45th AIAA/ ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA, Denver, Colorado, USA, 2009.
- Chern, J. S., Wu, B., Chen, Y. S. and Wu, A. M., "Suborbital and Low-Thermospheric Experiments Using Sounding Rockets in Taiwan", Acta Astronautica, Vol. 70, 2012, pp. 159-164. doi: 10.1016/j.actaastro.2011.07.030
-
Heo, J. Y., Cho, M. G., Park, H. J., Kim, S. J., Moon, H. J., Kim, J. K. and Sung, H. G., "Integrated Design of a Hybrid Sounding Rocket Using Liquid
$N_2O$ ", 2009 Asia-Pacific International Symposium on Aerospace Technology, JSASS, Gifu, Japan, 2009. - Dos Santos, L. M. C., de Almeida, L. A. R. and Veras, C. A. G., "Design and Flight Test of a Paraffin Based Hybrid Rocket", 18th International Congress of Mechanical Engineering, COBEM 2005, Minas Gerais, Brazil, 2005.
- Brooks, M. J., Pitot, J., Chowdhury, S. M., Genevieve, B. and Roberts, L. W., "Introduction to the University of KwaZulu-Natal Hybrid Sounding Rocket Program", 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA, Tennessee, USA, 2010.
- Tran, P. H. N., Booth, M. J., Robinson, J. H., Deyerle, L., Tarasi, N., Forster, Z. and Wirz, R., "Development and Test of an Experimental Hybrid Sounding Rocket", 8th Intercollegiate Rocket Engineering Competition, ESRA, Utah, USA, 2013.
-
McCormick, A., Hultgren, E., Lichtman, M., Smith, J., Sneed, R. and Azimi, S., "Design, Optimization, and Launch of a 3'' Diameter
$N_{2}O$ /Aluminized Paraffin Rocket", 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA, Arizona, USA, 2005. - Potter, C. R., Design of Economical Upper Stage Hybrid Rocket Engine, University of Tennessee Honors Thesis Projects, Tennessee, USA, 2013.
- Sako, N., Tsuda, Y., Ota, S., Eishima, T., Yamamoto, T., Ikeda, I., li, H., Yamamoto, H., Tanaka, H., Tanaka, A. and Nakasuka, S., "Cansat Suborbital Launch Experiment - University Educational Space Program Using can Sized pico-Satellite", Acta Astronautica, Vol. 48, No. 5-12, 2001, pp. 767- 776. doi: 10.1016/S0094-5765(01)00039-X
- Huzel, D. K. and Huang, D. H., Modern Engineering for Design of Liquid-Propellant Rocket Engines, AIAA, Washington DC, 1992.
- Sutton, G. P. and Biblarz, O., Rocket Propulsion Elements 8th ed., John wiley and sons, New Jersey, 2010.
- Chiaverini, M. J. and Kuo, K. K., Fundamentals of Hybrid Rocket Combustion and Propulsion, AIAA, Virginia, USA, 2007.
- Ribovich, J., Murphy, J. and Watson, R., "Detonation Studies with Nitric Oxide, Nitrous Oxide, Nitrogen Tetroxide, Carbon Monoxide, and Ethylene", Journal of Hazardous Materials, Vol. 1, No. 4, 1975, pp. 275-287. doi: 10.1016/0304- 3894(75)80001-X
-
Toussaint, M., Cesco, N., Masson, F., Theron, M., Iannetti, A., Verberne, O., Valle, T. R., Ronningen, J. E., Husdal, J., Lindstrom, B., Egnell, M. and Edlen, H., "Development Status of the 200N
$H_{2}O_{2}$ Thruster for a A5-ME Upper Stage Reaction Control System", SPACE PROPULSION 2014, Propulsion2014, Cologne, Germany, 2014. - Lee, M., Design and Performance Evaluation of Hdrogen Peroxide Oxidizer Hybrid Thruster for Sounding Rocket System, Master thesis, KAIST, Daejeon, South Korea, 2014.
- Jung, E. and Kwon, S., "Autoignitable and Restartable Hybrid Rockets Using Catalytic Decomposition of an Oxidizer", Journal of Propulsion and Power, Vol. 30, No. 2, 2014, pp. 514-517. doi: 10.2514/1.B34739
- Tsohas, J., Doppers, L. J., IV, E. G. C., Dambach, E. M. and Heister, S. D., "Progress in Technology Demonstration for a Small Hybrid Launch Vehicle", 5th Responsive Space Conference, AIAA, Los Angeles, CA, USA, 2007.
- Plumlee, D. and Steciak, J., "Development and Simulation of an Embedded Hydrogen Peroxide Catalyst Chamber in Low-Temperature Co-fired Ceramics", International Journal of Applied Ceramic Technology, Vol. 4, No. 5, 2007, p. 9. doi: 10.1111/j.1744-7402.2007.02161.x
- Pasini, A., Torre, L., Romeo, L., Cervone, A. and d'Agostino, L., "Performance Characterization of Pellet Catalytic Beds for Hydrogen Peroxide Monopropellant Rocket", Journal of Propulsion and Power, Vol. 27, No. 2, 2011, pp. 428-436. doi: 10.2514/1.B34000
- Lee, J. and Kwon, S., "Evaluation of Ethanol-Blended Hydrogen Peroxide Monopropellant on a 10 N Class Thruster", Journal of Propulsion and Power, Vol. 29, No. 5, 2013, pp. 1164-1170. doi: 10.2514/1.B34790
- Huh, J. and Kwon, S., "Design, Fabrication and Thrust Measurement of a Micro Liquid Monopropellant Thruster", Journal of Micromechanics and Microengineering, Vol. 24, No. 10, 2014, p. 9. doi: 10.1088/0960-1317/24/10/104001
-
An, S. and Kwon, S., "Scaling and Evaluation of
$Pt/Al_{2}O_{3} $ Catalytic Reactor for Hydrogen Peroxide Monopropellant Thruster", Journal of Propulsion and Power, Vol. 25, No. 5, 2009, pp. 1041-1045. doi: 10.2514/1.40822 -
Tian, H., Zhang, T., Sun, Z., Liang, D. and Lin, L., "Performance and Deactivation of Ir/
${\gamma} -Al_2O_3$ Catalyst in the Hydrogen Peroxide Monopropellant Thruster", Applied Catalysis A: General, Vol. 210, No. 1-2, 2001, pp. 55-62. doi: 10.1016/S0926-860X(00)00829-2 - An, S., Jo, S., Wee, J., Yoon, H. and Kwon, S., "Preliminary Flight Test of Hydrogen Peroxide Retro-Propulsion Module", Acta Astronautica, Vol. 67, No. 5-6, 2010, pp. 605-612. doi: 10.1016/j.actaastro.2010.04.010
-
Jang, D., Kang, S. and Kwon, S., "Preheating Characteristics of
$H_{2}O_{2}$ Monopropellant Thruster Using Manganese Oxide Catalyst", Aerospace Science and Technology, Vol. 41, 2015. doi: 10.1016/j.ast.2014.12.010 - Jang, D., Kwon, S. and Jo, S., "Effect of Phosphate Stabilizers in Hydrogen Peroxide Decomposition on Manganese-Based Catalyst", Journal of Propulsion and Power, Vol. 31, No. 3, 2015, pp. 904-911. doi: 10.2514/1. B35310
-
An, S., Design of
$H_2O_2$ Monopropellant Thruster with Consideration of Response Characteristics for Attitude Control System, Doctoral Dissertation, KAIST, Deajeon, South Korea, 2010. - Gordon, S. and McBride, B. J., "Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications", NASA Reference Publication 131, Cleveland, Ohio, 1994.
- Barrowman, J. S., The Practical Calculation of the Aerodynamic Characteristics of Slender Finned Vehicles, MSc, The Catholic University of America, Washington, D.C., USA, 1967.
- Barrowman, J. S. and Barrowman, J. A., "The Theoretical Prediction of the Center of Pressure", National Associatino of Rocketry, NARAM-8, 1966.
- Stine, G. H. and Stine, B., Handbook of Model Rocketry, Wiley, New Jersey, USA, 2004.
- Barrowman, J. S., "Calculating the Center of Presure", ESTES TIR-33, 1988.
- Niskanen, S., Development of an Open Source Model Rocket Simulation Software, Masters thesis, Helsinki University of Technology, Espoo, Finland, 2009.
피인용 문헌
- Preliminary Assessment of Hydrogen Peroxide Gel as an Oxidizer in a Catalyst Ignited Hybrid Thruster vol.2018, pp.1687-5974, 2018, https://doi.org/10.1155/2018/5630587