초록

우주비행체 추진기관은 로켓엔진의 일종으로 인공위성, 우주탐사선 등의 임무수행을 위해 사용되며 인공위성 자세제어 및 궤도조정을 위한 수요에 따라 1950년대 말부터 개발되기 시작하였다. 우주비행체에 사용되는 추진시스템은 발사체와 달리 상대적으로 긴 기간의 임무수행이 요구되며, 이에 따라 추진제의 안정성 및 추진시스템의 내구성이 설계에 매우 중요한 요소가 된다. 최근에 우주추진 분야에서 주목받는 기술은 이온성 액체를 이용한 친환경 추진과 전기추진만으로 추진시스템을 구성하는 기술로 국내에서도 체계적인 연구개발이 필요하다. 본 논문에서는 우주추진기관의 국내외 현황 및 주목받는 기술들을 나열하고 이에 따른 개발 전망을 간략히 소개하였다.

Abstract

Spacecraft propulsion system is a kind of rocket engine that has been developed from the end of 1950s for attitude control and orbit maintenance of satellite. Since the spacecraft propulsion system has to be used for a relatively long time, therefore, stability of propellant and life of thruster could be very important factor for propulsion system design. Recently, green propellant propulsion and all electrical propulsion system have became very important issue, and we also need a development according to well organized plan. In this paper, we will introduce the development status, key technologies and development prospect of spacecraft propulsion system.

주제어

#우주 추진   #화학 추진   #친환경 추진제   #하이드라진   #전기 추진  

참고문헌 (27)

1. Sutton, G. P., Rocket Propulsion Elements, John Wiley & Sons, 1992. 
2. Turner, M. J. L., Rocket and Spacecraft Propulsion, Springer, 2004. 
3. Han, C. Y., Kim, S. K. and Won, S. H. and Chae, J. W., "Monopropellant Thrusters for a Satellite," Current Industrial and Technological Trends in Aerospace, 2013, Vol. 11, No. 2, pp. 116-123. 
4. https://www.rocket.com/propulsion-systems/monopropellant-rockets 
5. http://www.moog.com/products/thrusters/ 
6. http://www.space-propulsion.com/spacecraft-propulsion/hydrazine-thrusters/index.html 
7. http://www.rafael.co.il/Marketing/422-1216-en/Marketing.aspx 
8. https://www.ihi.co.jp/ia/en/product/spp_b_02.html 
9. Kim, S. K. and Won, S. H., "Development of Monopropellant Thruster for Spacecraft Propulsion System," 45th KOSCO Symposium, 2012, pp. 295-296. 
10. Kim, S. K., Won, S. H., Kam, H. D., Lee, J. H., Lee, J. W. and Jun, H. Y., "A Development of 30N Class Hydrazine Thruster DM," 2015 KSPE Fall Conference, 2015. 
11. Anflo, K. and Crowe, B., "In-Space Demonstration of High Performance Green Propulsion and its Impact on Small Satellite," 25th Annual AIAA/USU Confere nce on Small Satellite, SSC11-IX-2, 2011. 
12. Spores, R. A., Masse, R., Kimbrel, S. and McLean, C., "GPIM AF-M315E Propulsion System," 49th AIAA/ASME/SAE/ ASEE Joint Propulsion Conference and Exhibit, AIAA 2013-3849, 2013. 
13. Tanaka, N., Matsuo T., Furukawa, K., Nishida, M., Suemori, S. and Yasutake, A., "The "Greening" of Spacecraft Reaction Control System," Mitsubishi Heavy Industries Technical Review, 2011, Vol. 48, No. 4, pp. 44-50. 
14. Fukuchi, B. A., Nagase, S., Maruizumi, H. and Ayabe, M., "HAN/HN-Based Monopropellant Thrusters," IHI Engineering Review, 2010, Vol. 43, No. 1, pp. 22-29. 
15. Zheng, H., Li, F., Zhang, S., Yu, X., Zhang, W. and Yao, Z., "Midinfrared Absorption Measurements of Nitrous Oxide in Ammonium Dinitramide Monopropellant Thruster," Journal of Propulsion and Power, 2015, Vol. 31, No. 5, pp. 1496-1500. 
16. Han, C. Y. and Chae, J. W., "Bipropellant Liquid Apogee Engine for a GEO Satellite," 2013 KSPE Fall Conference, 2013. 
17. http://www.northropgrumman.com 
18. Goebel, D. M. and Katz, I., Fundamentals of Electric Propulsion, John Wiley & Sons, 2008. 
19. Edwards, C. H., Wallac, N. C., Tato, C. and Put, P., "The T5 Ion Propulsion Assembly for Drag Compensation on GOCE," Proc. Second International GOCE User Workshop, 2014. 
20. The Annual Compendium of Commercial Space Transportation: 2014 
21. http://boeing.mediaroom.com/2014-11-12-oeing-tacks-Two-Satellites-to-Launch-as-a-Pair#ssets_117 
22. Goebel, D. M., Polk, J. E., Sandler, I., Mikellides, I. G., Brophy, J. R., Tighe, W. G. and Chien, K. R., "Evaluation of 25-cm XIPS Thruster Life for Deep Space Mission Applications," IEPC-2009-152, 2009. 
23. http://www.busek.com 
24. Mitrofanova, O. A., Gnizdor, R. Y., Murashko, V. M., Koryakin, A. I. and Nesterenko, A. N., "New Generation of SPT-100," IEPC-2011-041, 2011. 
25. http://www.space-propulsion.com/spaceraft-propulsion/ion-propulsion/index.html 
26. Kang, S. M., Kim, Y. H., Seon, J. H., Lee, J. S., Seo, M. H. and Choe, W. H., "Development of the Head Unit of a 300W Cylinderical Hall Thruster for Small Satellite," Journal of The Korean Society for Aeronautical and Space Sciences, 2009, Vol. 37, No. 5, pp. 496-501. 
27. Kim, S. K., Yu, M. J. and Choi, S. W., "Preliminary Design of ECR Ion Thruster," Aerospace Engineering and Technology, 2010, Vol. 9, No. 2, pp. 14-21. 

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