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Journal of the Korean Society of Propulsion Engineers - Vol. 24 , No. 6

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1. p. 1 Analysis of Pintle Tip Thermal Damage in the Combustion Hot Firing Test with a 1.5-tonf Class Liquid-Liquid Pintle Injector

Donghyuk Kang, Dokeun Hwang, Chulsung Ryu, Youngsung Ko
DOI: https://doi.org/10.6108/KSPE.2020.24.6.001

2. p. 10 A study on the Properties of Solid Propellant Containing FeOOH Combustion Catalyst: Effect of FeOOH Calcination Temperature

Su-A Jeon, Sung-Jun Park, Woon-Jae Kim, Jung-ho Park
DOI: https://doi.org/10.6108/KSPE.2020.24.6.010

3. p. 16 Design Method of 2D Scramjet Inlet Considering Wide Flight Range

Jaewon Lee, Sang Hun Kang
DOI: https://doi.org/10.6108/KSPE.2020.24.6.016

4. p. 28 Numerical Study on Transfer Port Design for Scavenging Performance in Small Two-stroke Engines

Cheonghwan Kim, Sungho Park, Myeongkyu Kim, Eunsoo Ahn
DOI: https://doi.org/10.6108/KSPE.2020.24.6.028

5. p. 45 Design for a Subminiature Solid Rocket Motor

Sunyoung Lee, Hyunseob Lee, Heeseong Yang, Taeock Khil, Dongwook Kim, Jaehoon Bang, Sungho Choi, Yongseon Lee
DOI: https://doi.org/10.6108/KSPE.2020.24.6.045

6. p. 53 Effects of Ultrasonic Standing Wave on the Ultrasonically-atomized Aerosol Flame Injected through a Slit-jet Nozzle

Hyun Jong Ahn, Yun Hyeong Kang, Jeong Soo Kim
DOI: https://doi.org/10.6108/KSPE.2020.24.6.053

7. p. 61 High Frequency Signal Analysis of Oxidizer Pump for 7-tonf Turbopump

Joon-Hwan Bae, Chang-Ho Choi, Jong-Soo Choi
DOI: https://doi.org/10.6108/KSPE.2020.24.6.061

8. p. 69 Performance Analysis of Liquid Pintle Thruster Using Quasi-one-dimensional Multi-phase Reaction Flow: Part I Key Sub-model Validation

Jeongseok Kang, Janghan Bok, Hong-Gye Sung, Minchan Kwon, JunYoung Heo
DOI: https://doi.org/10.6108/KSPE.2020.24.6.069

9. p. 78 Performance Analysis of Liquid Pintle Thruster Using Quasi-one-dimensional Multi-phase Reaction Flow: Part II. Thruster Performance Characteristics

Jeongseok Kang, Janghan Bok, Hong-Gye Sung, Minchan Kwon, JunYoung Heo
DOI: https://doi.org/10.6108/KSPE.2020.24.6.078

10. p. 85 A Comparative Analysis for the Performance of 200 N-class Gaseous Methane-Liquid Oxygen Small Rocket Engine According to the Characteristic Length Variation

Yun Hyeong Kang, Hyun Jong Ahn, Jeong Soo Kim
DOI: https://doi.org/10.6108/KSPE.2020.24.6.085

11. p. 93 Operational Characteristic of Liquid Rocket Engine by Cavitation Instability at Low Inlet Pressure Condition

Dae-Jin Kim, Byung Yun Kang, Chang-Ho Choi
DOI: https://doi.org/10.6108/KSPE.2020.24.6.093

12. p. 101 The Study of Curing Day Reduction by Step Curing of HTPB/AP Propellant

Kahee Kim, Jung-Ho Park, Sunghan Choi
DOI: https://doi.org/10.6108/KSPE.2020.24.6.101

13. p. 108 Feasibility Study of the Application of Infinite Tube Probe in High Temperature Environment

Hyeonjun Kim, Chulsung Ryu
DOI: https://doi.org/10.6108/KSPE.2020.24.6.108

14. p. 120 Pressure Drop Changes at Engine Fuel Inlet Filter according to Water Contents Management of KSLV-II Liquid Rocket Fuel

Changhwan Hwang, Inho Kim, Jaeyoung Park, Seonglyong Kim, Byungil Yoo, Namkyung Cho, Yeoungmin Han
DOI: https://doi.org/10.6108/KSPE.2020.24.6.120

15. p. 126 Analysis on the Research and Development Cases of Combustion Devices with Liquid-Liquid Pintle Injector

DoKeun Hwang, Chulsung Ryu, Sejin Kwon
DOI: https://doi.org/10.6108/KSPE.2020.24.6.126

16. p. 143 Modeling and Validation of a Liquid Propellant Supply System in Steady States

Juyeon Lee, Wonkeun Ki, Hwanil Huh, Tae-seong Roh, Hyoung Jin Lee
DOI: https://doi.org/10.6108/KSPE.2020.24.6.143

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