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1. p. 1 Comparative Evaluation on the Deriving Method of the Heat Transfer Coefficient of the C-D Nozzle
Tae Won Noh, Tae-Seong Roh, Hyoung Jin Lee, Hyunseob Lee, Phil Hoon Yoo
DOI: https://doi.org/10.6108/KSPE.2022.26.2.001 |
2. p. 12 Burn-back Analysis for Propellant Grains with Embedded Metal Wires
Hyunseob Lee, Jongyun Oh, Heesung Yang, Sunyoung Lee, Taeock Khil
DOI: https://doi.org/10.6108/KSPE.2022.26.2.012 |
3. p. 20 Non-ignition Evaluation Method for Hypergolic Propellant Using Microreactor
Kyounghwan Lee, Seonghyeon Park, Hongjae Kang, Jongkwang Lee
DOI: https://doi.org/10.6108/KSPE.2022.26.2.020 |
5. p. 40 Development of Sub-200 W Laboratory Model Hall Thrusters for Small and Micro Satellites
Dongho Lee, Holak Kim, Guentae Doh, Youngho Kim, Jaehong Park, Jaejun Lee, Wonho Choe
DOI: https://doi.org/10.6108/KSPE.2022.26.2.040 |
6. p. 47 Liquid Hydrogen/Liquid Oxygen Rocket Engine Technology
Nam-Kyung Cho, Soon-Young Park, Seong-Han Kim, Yeong-Min Han
DOI: https://doi.org/10.6108/KSPE.2022.26.2.047 |
7. p. 60 High Pressure Spray and Combustion Characteristics of Throttleable Pintle Injector
Dae Hwan Kim, Subeom Heo, Inho Kim, Donghyun Hwang, Cheolwoong Kang, Shinwoo Lee, Kyubok Ahn, Youngbin Yoon
DOI: https://doi.org/10.6108/KSPE.2022.26.2.060 |
8. p. 72 Design and Pressure Loss Evaluation of Vacuum Brazed Cooling Passage for Full Authority Digital Engine Control
Myeongjae Han, Jinwoon Seol, Seungho Jeong, Minkyung Cha, Hoyoun Jang, Junghoe Kim
DOI: https://doi.org/10.6108/KSPE.2022.26.2.072 |
9. p. 79 Trend Analysis in Upper Stage Engine Development of Space Launch Vehicles
Kyunghwan Han, Tae-Seong Rho, Hwanil Huh, Hyoung Jin Lee
DOI: https://doi.org/10.6108/KSPE.2022.26.2.079 |