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2025 Vol.29, Issue 6 Preview Page

RESEARCH PAPERS

31 December 2025. pp. 7-14
Abstract
References
1

Park, I., Kim, C., and Kim, J., “A Trend Analysis and Future Opportunities on the Solid Fuel Ramjet Technology,” Journal of the Korean Society of Propulsion Engineers, Vol. 28, No. 3, 2024, pp. 128-146.

10.6108/KSPE.2024.28.3.128
2

Hedman, T. D., “Radiation-induced pyrolysis of solid fuels for ramjet application,” Propulsion and Power Research, Vol. 5, No. 2, 2016, pp. 87-96.

10.1016/j.jppr.2016.04.002
3

Jung, W., Lee, J., Jeon, S., Park, S., and Kwon, S., “Combustion test of solid fuel ramjet combustor using gas generator,” In 53rd AIAA/SAE/ASEE Joint Propulsion Conference, Atlanta, USA, Jul 10-12, 2017.

10.2514/6.2017-4945
4

McDonald, B., Krishnan, S., Higa, K., and Manginell, R., “High density solid fuel ramjet fuel based on 1, 6-hexanediol diglycidyl ether and methyltetrahydrophthalic anhydride,” Fuel, Vol. 278, 2020, p. 118354.

10.1016/j.fuel.2020.118354
5

Krishnan, S., “Solid-Fuel Ramjet Assisted Gun-Launched Projectiles: An Overview,” Proceedings of 5th National Conference on Airbreathing and Aerospace Propulsion, Hyderabad, India, pp. 1-21, Dec 2000.

6

Oosthuizen, R., Buisson, J. J., and Botha, G. F., “Solid Fuel Ramjet Propulsion for Artillery Projectile Applications – Concept Development Overview,” Proceedings of the 19th International Symposium of Ballistics, Interlaken, Switzerland, pp. 403-410, May 2001.

7

Dionisio, F., and Stockenstrom, A., “Aerodynamic Wind-tunnel Test of a Ramjet Projectile,” Proceedings of the 19th International Symposium of Ballistics, Interlaken, Switzerland, pp. 529-536, May 2001.

8

Kim, C., “Performance Evaluation of Small Solid Fuel Ramjet Engine Using Direct-Connect Test,” Proceedings of the Korean Society for Aeronautical & Space Sciences Conference, Jeju, Korea, Oct 2023.

9

Zarko, V., Kiskin, A., and Cheremisin, A., “Contemporary methods to measure regression rate of energetic materials: A review,” Progress in Energy and Combustion Science, Vol. 91, 2022, p. 100980.

10.1016/j.pecs.2021.100980
10

Hasegawa, K., and Hori, K., “Novel burning rate measurement technique for solid propellant by means of ultrasonics,” Combustion, Explosion, and Shock Waves, Vol. 46, 2010, pp. 188-195.

10.1007/s10573-010-0029-1
11

McQuade, W., Parr, T., Boon, J., and Jurick, D., “Determination of the ultrasonic burning rate technique resolution,” In 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cleveland, USA, Jul 1998.

10.2514/6.1998-3555
12

Song, S. J., Kim, Y. J., Kim, H. J., and Park, J. H., “Measurement of solid propellant burning rates by analysis of ultrasonic full waveforms,” Journal of Mechanical Science and Technology, Vol. 23, 2020, pp. 1112-1117.

10.1007/s12206-009-0302-y
13

Deepak, D., Jeenu, R., Sridharan, P., and Padmanabhan, M., “Application of Ultrasonic Technique for Measurement of Instantaneous Burn Rate of Solid Propellants,” Defence Science Journal, Vol. 48, 2013, pp. 197-204.

10.14429/dsj.48.3899
14

Wu, P., Longworth, D., and Whitney, D., “Development of an ultrasonic burning rate measurement technique,” In 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, Alabama, USA, Jul 2003.

10.2514/6.2003-5181
15

Kurabayashi, H., Fujii, M., Tani, K., and Kawai, Y., “Ultrasonic measurements of burning rates in full-size rocket motors,” Progress in Propulsion Physics, Vol. 2, 2011, pp. 135-148.

10.1051/eucass/201102135
16

Porrmann, D., Haucke, C., Woeste, L., Fiedler, T., and Hauth, J., “First Results of Regression Rate Measurements on Ultrasonic Basis in the Ahres Hybrid Rocket Motor,” In 2nd CEAS Space Conference, Köln, Deutschland, Germany, May 2014.

17

Evans, J. V., “Experimental Measurement and Modeling of Regression Rate Phenomena in Solid Fuel Ramjet Combustors,” Ph.D. Dissertation, School of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana, USA, 2023.

18

Park, J. W., Ku, K. W., Hong, J. G., and Lee, C. W., “Study on the Measurement Techniques of Solid Fuel Regression Rate in Hybrid Rocket,” Proceedings of the Korean Society of Mechanical Engineers Annual Conference, Jeju, Korea, Nov 2010.

19

Song, S. J., Ko, S. F., Kim, H. J., Oh, H. T., Kim, I. C., Yoo, J. C., and Jung, J. Y., “Burning Rate Testing of Double Base Solid Propellants using Ultrasound,” Journal of the Korean Society of Propulsion Engineers, 2006, pp. 247-250.

20

Kang, T., Song, S. J., Kim, H. J., Ko, S. F., Oh, H. T., Kim, I. C., Yoo, J. C., and Jung, J. Y., “Evaluation of Uncertainty in Burning Rate Measurement of Solid Propellant using Ultrasound,” Journal of the Korean Society of Propulsion Engineers, 2008, pp. 199-202.

21

Oh, H. T., Song, S. J., Kim, H. J., Ko, S. F., Kim, I. C., Yoo, J. C., and Jung, J. Y., “Analysis of Measurement Accuracy up to High Pressure for Various Solid Propellants using Ultrasound,” Journal of the Korean Society of Propulsion Engineers, 2008, pp. 265-268.

22

Lim, S., and Kim, D., “A Study on Ultrasonic Wave Propagation Model in Multi-Layer Media,” Journal of the Korean Society of Propulsion Engineers, Vol. 16, No. 3, 2012, pp. 9-15.

10.6108/KSPE.2012.16.3.009
23

Yun, L., Kim, D., Park, I., Han, S., and Sim, H. S., “Ultrasonic Signal Analysis of Solid Propellant Using Hilbert Transform,” Journal of the Korean Society of Propulsion Engineers, Vol. 28, No. 4, 2024, pp. 20-28.

10.6108/KSPE.2024.28.4.020
24

Jung, S. M., and Yoon, J. S., “Review of Ultrasonic Techniques for Measuring Solid Propellant Burning Rate,” Journal of the Korean Society of Propulsion Engineers, 2021, pp. 36-41.

25

Guerra, A. S., “Fuel Regression Studies of a Miniature Optically Accessible Solid Fuel Ramjet Slab Burner,” M.S. Thesis, Department of Mechanical and Aerospace Engineering, California State University, Long Beach, USA, 2022.

Information
  • 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 : 29
  • No :6
  • Pages :7-14
  • Received Date : 2025-07-07
  • Revised Date : 2025-08-28
  • Accepted Date : 2025-09-04