TECHNICAL PAPERS
Marshall, W. M. and Deans, M. C., "Recommended Figures of Merit for Green Monopropellants," 49th AIAA/ASME/SAE/ ASEE Joint Propulsion Conference and Exhibit, San Jose, C.A., U.S.A., AIAA 2013-3722, Jul. 2013.
10.2514/6.2013-3722Sutton, G. P. and Biblarz, O., Rocket Propulsion Elements, 9th ed., John Wiley & Sons Inc., New York, N.Y., U.S.A, 2016.
Russi, M., "A Survey of Monopropellant Hydrazine Thruster Technology," 9th Propulsion Conference, Las Vegas, N.V., U.S.A, Nov. 1973.
10.2514/6.1973-1263Roe, F. J. C., Grant, G. A., and Millican, D. M., "Carcinogenicity of Hydrazine and 1, 1-dimethylhydrazine for Mouse Lung," Nature, Vol. 216, pp. 375-376, 1967.
10.1038/216375a06053815Whitmore, S. A., Merkley, D. P., Judson, M. I., and Eilers, S. D., "Development and Testing of a Green Monopropellant Ignition System," 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, San Jose, C.A., U.S.A., AIAA 2013-3967, Jul. 2013.
10.2514/6.2013-3967Simpson, D. K., "Safety and Handling of Hydrazine," Olin Corp Cheshire CT Olin Research Center AD-P005, 1986.
Jankovsky, R., "HAN-based Monopropellant Assessment for Spacecraft," 32nd Joint Propulsion Conference and Exhibit, Lake Buena Vista, F.L., U.S.A., AIAA 1996-2863, Jul. 2013.
10.2514/6.1996-28638693670Anflo, K., Gronland, T., and Wingborg, N. "Development and Testing of ADN-based Monopropellants in Small Rocket Engines," 36th AIAA/ASME/SAE /ASEE Joint Propulsion Conference and Exhibit, Las Vegas, N.V., U.S.A., AIAA 2000-3162, Jul. 2000.
10.2514/6.2000-3162Gohardani, A. S., Stanojev, J., Demairé, A., Anflo, K., Persson, M., Wingborg, N., and Nilsson, C., "Green Space Propulsion: Opportunities and Prospects," Progress in Aerospace Sciences, Vol. 71, pp. 128-149, 2014.
10.1016/j.paerosci.2014.08.001Wingborg, N., "Heat of Formation of ADN Based Liquid Monopropellants," Propellants, Explosives, Pyrotechnics, Vol. 44, pp. 1090- 1095, 2019.
10.1002/prep.201900142Anflo, K., and Möllerberg, R, "Flight Demonstration of New Thruster and Green Propellant Technology on the PRISMA Satellite," Acta Astronautica, Vol. 65, pp. 1238-1249, 2009.
10.1016/j.actaastro.2009.03.056Anflo, K., and Crowe, B., "In-space Demonstration of an ADN-based Propulsion System," 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, San Diego, C.A., U.S.A., AIAA 2011-5832, Jul. 2011.
10.2514/6.2011-5832Kim, J. W., Baek, S., Jung, Y., Yoon, W., Ban, H. S., and Kwon, S., "An Alternative ADN Based Monopropellant Mixed with Tetraglyme," Acta Astronautica, Vol. 178, pp. 241-249, 2021.
10.1016/j.actaastro.2020.09.007Kim, J. W., Bhosale, V. K., Kim, K. S., Lee, S., and Kwon, S, "Room-temperature Catalytically Reactive Ammonium Dinitramide- H2O2 Monopropellant for Microsatellites," Advances in Space Research, Vol. 69, pp. 1631-1644, 2022.
10.1016/j.asr.2021.11.022Wilhelm, M., Negri, M., Ciezki, H., and Schlechtriem, S., "Preliminary Tests on Thermal Ignition of ADN-based Liquid Monopropellants," Acta Astronautica, Vol. 158, pp. 388-396, 2019.
10.1016/j.actaastro.2018.05.057Khare, P., Yang, V., Meng, H., Risha, G. A., and Yetter, R. A., "Thermal and Electrolytic Decomposition and Ignition of HAN-water Solutions," Combustion Science and Technology, Vol. 187, pp. 1065-1078, 2015.
10.1080/00102202.2014.993033Park, K., and Kim, T., "Experimental Studies on Effects of Electrode Material and Voltage on Electrolytic Decomposition of Hydroxylammonium Nitrate Solution," Acta Astronautica, Vol. 216, pp. 267-274, 2024.
10.1016/j.actaastro.2024.01.008Lani, B. P., "Microwave Ignition of Green Monopropellants," Master of Science Thesis, Aerospace Engineering Dept., The Pennsylvania State University, 2014.
Auman, K., "Non-Catalytic Microwave Ignition of Green Hydrazine Replacements," Master of Science Thesis, Aerospace Engineering Dept., The Pennsylvania State University, 2019.
Finke, T., "Non-Catalytic Microwave Ignition of Green Hydrazine Replacements," Air Force Life Cycle Management Center, WP18-1661, 2020.
Thrasher, J., Williams, S., Takahashi, P., and Sousa, J., "Pulsed Plasma Thruster Development Using A Novel HAN-Based Green Electric Monopropellant," 52nd AIAA/ SAE/ASEE Joint Propulsion Conference, Salt Lake City, U.T., U.S.A., AIAA 2016- 4846, Jul. 2016.
10.2514/6.2016-4846Kakami, A., Yamamoto, N., Ideta, K., and Tachibana, T. "Design and Experiments of a HAN-based Monopropellant Thruster Using Arc-discharge Assisted Combustion," Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 10, pp. Pa_13-Pa_17, 2012.
10.2322/tastj.10.Pa_13Kakami, A., Ideta, K., Ishibashi, T., and Tachibana, T., "One Newton Thruster by Plasma-assisted Combustion of HAN-based Monopropellant," 48th AIAA/ASME/SAE/ ASEE Joint Propulsion Conference and Exhibit, Atlanta, G.A., U.S.A., AIAA 2012-3756, Jul. 2012.
10.2514/6.2012-3756Iizuka, T., Shindo, T., Wada, A., Kawabata, S., Sato, Y., Aoyagi, J., Takegahara, H., and Nagata, T., "Basic Characteristics of Discharge Plasma Ignition System for 1N-Class RCS Thruster with Green Monopropellant," 50th AIAA/ASME/SAE/ ASEE Joint Propulsion Conference, Cleveland, O.H., U.S.A., AIAA 2014-3885, Jul. 2014.
10.2514/6.2014-3885Wada, A., Iizuka, T., Shindo, T., Maeda, H., Watanabe, H., and Takegahara, H., "Effect of Geometric Swirl Number of Discharge Plasma Catalyzer on Green Monopropellant Reaction Characteristics," Transactions of the Japan Society for Aeronautical and Space Sciences, vol. 14, pp. Pa_139-Pa_144, 2016.
10.2322/tastj.14.Pa_139Wada, A., Watanabe, H., and Takegahara, H., "Performance Evaluation of a Hydroxy- lammonium-Nitrate-Based Monopropellant Thruster with Discharge Plasma System," 53rd AIAA/SAE/ASEE Joint Propulsion Conference, Atlanta, G.A., U.S.A., AIAA 2017-4757, Jul. 2017.
10.2514/6.2017-4757Wada, A., Watanabe, H., and Takegahara, H., "Combustion Characteristics of a Hydroxy- lammonium-nitrate-based Monopropellant Thruster with Discharge Plasma System," Journal of Propulsion and Power, vol. 34, pp. 1052-1060, 2018.
10.2514/1.B36762Shindo, T., Wada, A., Maeda, H., Watanabe, H., and Takegahara, H., "Influence of Design Factors on the Thrust Performance of a Green Monopropellant Reaction System with Plasma," Transactions of the Japan Society for Aeronautical and Space Sciences, vol. 60, pp. 103-108, 2017.
10.2322/tjsass.60.103Shindo, T., Wada, A., Maeda, H., Watanabe, H., and Takegahara, H., "Performance of a Green Propellant Thruster with Discharge Plasma," Acta Astronautica, Vol. 131, pp. 92-95, 2017.
10.1016/j.actaastro.2016.11.022Wada, A., and Habu, H., "Electric Ignition Characteristics of an Ammonium-dinitramide-based Ionic liquid Monopropellant with Discharge Plasma," AIAA Scitech 2020 Forum, Orlando, F.L., U.S.A., AIAA 2020-1895, Jan. 2020.
10.2514/6.2020-1895Tang, Y., Li, S., Yao, Z., Huang, B., and Li, S., "Ignition of an Ionic Liquid Dual- mode Monopropellant Using a Microwave Plasma Torch," Proceedings of the Combustion Institute, Vol. 39, pp. 5063-5071, 2023.
10.1016/j.proci.2022.09.003Kim, M., Choi, W., Bae, G. and Kim, T., "N2O-PMMA Ignition Assisted with Plasma," 2018 KSPE Spring Conference, Jeju, South Korea, KSPE 2018-1145, May. 2018.
Kim, M. and Kim, T., "Experimental Study of N2O Plasma Igniter for PMMA Combustion," Journal of the Korean Society of Propulsion Engineers, Vol. 23, No. 3, pp. 1-8, 2019.
10.6108/KSPE.2019.23.3.001- Publisher :The Korean Society of Propulsion Engineers
- Publisher(Ko) :한국추진공학회
- Journal Title :Journal of the Korean Society of Propulsion Engineers
- Journal Title(Ko) :한국추진공학회지
- Volume : 28
- No :3
- Pages :75-90
- Received Date : 2024-02-06
- Revised Date : 2024-03-30
- Accepted Date : 2024-04-03
- DOI :https://doi.org/10.6108/KSPE.2024.28.3.075


Journal of the Korean Society of Propulsion Engineers








