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2025 Vol.29, Issue 3 Preview Page

TECHNICAL PAPERS

30 June 2025. pp. 52-58
Abstract
References
1

Jin, J.K., Ha D.S. and Oh, S.J., "Experimental Study and Performance Analysis of the Solid Rocket Motor with Pintle Nozzle," Journal of the Korean Society of Propulsion Engineers, Vol. 20, No. 4, pp. 59-67, 2016.

2

Hopfe., N., Naumann, K.W., Caldas Pinto, P., Ramsel, J., Niedermaier, H. and Thumann., A., "Hot Gas Nozzle-Valve Assembly and Control Method for Continuously Operating Divert and Attitude Control Systems," AIAA Propulsion and Energy Forum, Indianapolis, IN, U.S.A., Aug. 2019.

10.2514/6.2019-3879
3

Heo, J.Y., Jung, J.Y., Sung, H.G., Yang, J.S. and Lee, J.L., "Compressibility Correction Effects of Two- equation Turbulence Models for a Supersonic Through-type Pintle Nozzle with Large Scale Separation Flow," Journal of the Korean Society of Propulsion Engineers, Vol. 17, No. 1, pp. 61-69, 2013.

10.6108/KSPE.2013.17.1.061
4

Lafond, A., "Numerical Simulation of the Flowfield Inside a Hot Gas Valve," 37th Aerospace Sciences Meeting and Exhibit, Reno, NV, U.S.A., AIAA 99-1087, Jan. 1999.

10.2514/6.1999-1087
5

Jin, J.K., Ha, D.S., Lee, J.S. and Ki, T.S., "Study of pintle-nozzle performance with CFD simulation," 44th KSPE Spring Conference, Jeju, Korea, pp. 684-688, May. 2015.

6

Kim, J.K., Lee, J.H. and Chang, H.B., "Computational Investigation of Pintle Nozzle Flow," Journal of the Korean Society of Propulsion Engineers, Vol. 13, No. 2, pp. 35-41, 2009.

7

Kim, J.K. and Park, J.H., "Thrust Modulation Performance Analysis of Pintle-nozzle Motor," Journal of the Korean Society for Aeronautical and Space Sciences, Vol. 37, No. 4, pp. 392-398, 2009.

10.5139/JKSAS.2009.37.4.392
8

Jeong, K.Y., Hong, J.S., Heo, J.Y., Sung, H.G., Yang, J.S. and Ha, D.S., "Thrust Characteristics of Through-type Pintle Nozzle at Operating Altitudes Condition," Journal of the Korean Society of Propulsion Engineers, Vol. 20, No. 4, pp. 59-67, 2016.

10.6108/KSPE.2016.20.4.059
9

Kim, J.K., Park, J.H., Lee, J.H. and Jeon, M.K., "A Study on the Pintle-tip Shapes Effect of Nozzle Flow Using Cold-flow Test," Journal of the Korean Society for Aeronautical and Space Sciences, Vol. 38, No. 10, pp. 985-991, 2010.

10.5139/JKSAS.2010.38.10.985
10

Kim, J.K., Lee, J.H., Oh, J.Y. and Chang, H.B., "A Study on Steady State Performance of Variable Thrust Nozzle by Cold-flow Test," Journal of the Korean Society of Propulsion Engineers, Vol. 12, No. 2, pp. 8-14, 2008.

11

Lim, S.T., Ha, D.S., Park, S.H. and Kim, Y.C., "Design and Fabrication of Hot Gas Components for DACS Applications," 42th KSPE Spring Conference, Jeju, Korea, pp. 308-312, 2014

12

Benner, M.S. and Sawyer, R.H., "Revised tables of airspeed, altitude, and Mach number presented in the international system of units", NASA-SP-3082, 1973.

13

Lee, J.M., Park, K.S., Ahn, D.C. and Jeong, H.S., "Test Results of High Altitude Test Facility with Steam Generators Connected in Parallel," 63th KSPE Spring Conference, Busan, Korea, Sep. 2024(to be published).

14

KALT, S. and Badal, D.L., "Conical Rocket Nozzle Performance Under Flow-separated Conditions," Journal of Spacecraft and Rockets, Vol. 2, No. 3, pp. 447-449, 1965.

10.2514/3.28200
15

NASA, "Solid Rocket Motor Performance Analysis and Prediction," NASA-SP-8039, p. 70, 1971.

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 :3
  • Pages :52-58
  • Received Date : 2024-12-16
  • Revised Date : 2025-04-18
  • Accepted Date : 2025-05-06