Acknowledgement
본 연구는 한국항공우주연구원 2단형 소형발사체선행기술개발사업(FR22B00)과 한국연구재단(과학기술정보통신부) 스페이스챌린지사업(2021M1A3B807777112) 지원을 받아 수행되었습니다.
References
- Lim, B., Kim, C. W., Lee, K. O., Lee, K., Park, J., Ahn, K., Namkoung, H. J. and Yoon, Y., "Development Trend of Liquid Methane Rocket Engine and Implications," Journal of the Korean Society of Propulsion Engineers, Vol. 25, No. 2, pp. 119-143, 2021. https://doi.org/10.6108/KSPE.2021.25.2.119
- Lim, B., Lim, H., Lee, K. and Park, J., "Testing an Additively Manufactured Thrust Chamber for 1-tonf Class Methane Engine," Proceeding of the 2021 KSPE Spring Conference, Jeju, Korea, pp. 339-405, May 2021.
- Lim, H., Lim, B., Shin, D., Lim, S., Lee, K. and Park, J., "Regenerative Cooled Firing Test of the 1-tonf Oxygen/Methane Thrust Chamber Manufactured Metal 3D Printing," Proceeding of the 2021 KSPE Fall Conference, Busan, Korea, KSPE 2021-2248, Nov. 2021.
- Roman, M., Andrii O., Samir, O., Mihaylo, A., and Olexander, B., "3D Printed Acoustic Igniter of Oxygen-Kerosene Mixtures for Aerospace Applications," 8th European Conference for Aeronautics and Space Sciences, Madrid, Spain, EUCASS2019-0238, Jul. 2019.
- Borner, M., Hardi, J., Suslov, D., Deeken, and Oschwald, M., "LUMEN Thrust Chamber - Ignition Characteristics and Thrust Chamber Transients," 32nd International Symposium on Space Technology and Science, Fukui, Japan, 2019-a-11, Jan. 2019.
- Thomas, F., Bernd, M., Gerhard, K., Klas, L., Arianna, D., Rudi, M., and Kate, U., "FLPP ETID: TRL6 reached for Enabling Technologies for Future European Upper Stage Engines," 8th European Conference for Aeronautics and Space Sciences, Madrid, Spain, EUCASS2019-0208, Jul. 2019.
- P. Sabin, A. Michallet, N. Meyers, S. Durteste, J.-F. Delange, S. Saubadine and J.M. Ruault, "VULCAIN®2.1, the European reference for Ariane 6 Lower stage cryogenic propulsive system," 8th European Conference for Aeronautics and Space Sciences, Madrid, Spain, EUCASS2019-0639, Jul. 2019.
- Hwang, D., Kim, H.J., Kim, J., Lim, B., Kim, M. and Choi, H. S., "A Configuration of Multiple Ignition Fuel Ampules for Thrust Chamber Hot-Firing Tests," Proceeding of the 2015 KSPE Spring Conference, Busan, Korea, pp. 747-750, May 2015.
- Lee, J., Jeon, J., Woo, S., Lee, K., Kim, S. and Han, Y., "Configuration and Pre-tests of Reignition System of Staged Combustion Cycle Engine," Proceeding of the 2021 KSPE Spring Conference, Jeju, Korea, KSPE 2021-1168, May 2021.
- "Multi-Ignition Equipment," retrieved on 29 Apr. 2022 from Korea On-line E-Procurement System (https://www.g2b.go.kr/index.jsp), notice no. 20220439975.
- Sebastian, S., Nico, R., and Gerhard, K., "Laser Ignition Application to Cryogenic Propellant Rocket Thrust Chambers," Laser Ignition Conference, Optical Society of America, Bucharest, Romania, LFA4-3, Jun. 2017.
- P. Sabin, A. Michallet, N. Meyers, S. Durteste, and J.-F. Delange, "Vulcain2.1, the European Reference for Ariane 6 Lower Stage Cryogenic Propulsive System," 8th European Conference for Aeronautics and Space Sciences, Madrid, Spain, EUCASS2019-0639, Jul. 2019.
- Paul, L., Christian, B., and Oscar, J. H., "Design Aspects and Characterisation of a Resonance Igniter for Oxygen/Methane in-Oribit Propulsion Systems," 8th European Conference for Aeronautics and Space Sciences, Madrid, Spain, EUCASS2019-0651, Jul. 2019.
- Bae, J. Y., Seo, S. and Kang, S. H., "Experimental Results of Thermoacoustic Resonance Heat Generation," Proceeding of the 2017 KSPE Spring Conference, Jeju, Korea, pp. 730- 733, May 2017.
- "Acoustic Igniter," retrieved on 29 April, 2022 from https://flightcontrolpropulsion.com.
- Lim, B., Lim, H. Y., Lee, K. and Park, J., "Testing an Additively Manufactured Thrust Chamber for 1-tonf Class Methane Engine," Proceeding of the 2021 KSPE Spring Conference, Jeju, Korea, pp. 399-405, May 2021.
- Lim, H. Y, Lim, B., Shin, D., Lim, S. S., Lee, K. and Park, J., "Regeneratively Cooled Firing Test of a 1-tonf Oxygen/ Methane Thrust Chamber Manufactured Metal 3D Printing," Proceeding of the 2021 KSPE Fall Conference, Busan, Korea, KSPE 2021-2248, Nov. 2021.
- Lim, B., Lee, K. and Park, J., "An Integrated, Multi-Ignition System Fed Solely by Main-Feedline Branches of Liquid Methane Rocket Engine," Proceeding of the Korean Society for Aeronautical and Space Sciences Spring Conference, Gosung, Korea, pp. 212-216, Apr. 2021.