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1 |
Determination of The Cryogenic Propellant Parameters at Pressurization of The Propulsion System Tank by Bubbling
Bershadskiy Vitaly A.;Jung, Young-Suk;Lim, Seok-Hee;Cho, Gyu-Sik;Cho, Kie-Joo;Kang, Sun-Il;Oh, Seung-Hyub;
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The Korean Society of Propulsion Engineers
, v.10, no.4, pp.1-10,
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2 |
Analysis on Two Parallel Flows in Convergent Channel
Kwon, Jin-Kyung;Kim, Tae-Wook;Kim, Jin-Hyun;Kim, Jae-Yeol;
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The Korean Society of Propulsion Engineers
, v.10, no.4, pp.11-18,
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3 |
Thermal Transient Characteristics of Initiator with STS 304 Bridgewire
Yoon, Ki-Eun;Ryu, Byung-Tae;Choi, Chang-Sun;
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The Korean Society of Propulsion Engineers
, v.10, no.4, pp.19-25,
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4 |
Spray and Combustion Characteristics of High Density Hydrocarbon Fuel
Lim, Byoung-Jik;Moon, Il-Yoon;Seo, Seong-Hyeon;Han, Yeoung-Min;Choi, Hwan-Seok;
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The Korean Society of Propulsion Engineers
, v.10, no.4, pp.26-33,
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5 |
Comparison of Forming force on forward and Backward Flow Forming for Combustion Chamber
Nam, Kyoun-Go;Cho, Cheon-Hwey;Hong, Sung-In;
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The Korean Society of Propulsion Engineers
, v.10, no.4, pp.34-39,
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6 |
Combustion Experiments of a High Pressure Liquid Propellant Thrust Chamber
Seo, Seong-Hyeon;Han, Yeoung-Min;Moon, Il-Yoon;Lee, Kwang-Jin;Kim, Jong-Kyu;Lim, Byung-Jik;Ahn, Kyu-Bok;Choi, Hwan-Seok;
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The Korean Society of Propulsion Engineers
, v.10, no.4, pp.40-46,
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7 |
3-D finite Element Analysis for Thermo-Mechanical Behavior of Laminated Carbon-Phenolic Composite Ring for Rocket Nozzle Insulator
Lee, Sun-Pyo;
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The Korean Society of Propulsion Engineers
, v.10, no.4, pp.47-53,
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8 |
A Study on Compressor Map Generation of a Gas Turbine Engine Using Hybrid Intelligent Method
Kong, Chang-Duk;Kho, Seong-Hee;Ki, Ja-Young;
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The Korean Society of Propulsion Engineers
, v.10, no.4, pp.54-60,
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9 |
The Principle and a Prototype System for Burning Rate Measurement of Solid Propellants Using Ultrasound
Song, Sung-Jin;Jeon, Jin-Hong;Kim, Hak-Joon;Oh, Hyun-Taek;Kim, In-Chul;Yoo, Ji-Chang;Jung, Jung-Yong;
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The Korean Society of Propulsion Engineers
, v.10, no.4, pp.61-68,
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10 |
Structural Analysis of Liquid Rocket Thrust Chamber Regenerative Cooling Channel using Bodner-Partom Viscoplastic Model
Ryu, Chul-Sung;Baek, Un-Bong;Choi, Hwan-Seok;
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The Korean Society of Propulsion Engineers
, v.10, no.4, pp.69-76,
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11 |
Design, Fabrication and Testing of Planar Type of Micro Solid Propellant Thruster
Lee, Jong-Kwang;Kwon, Se-Jin;
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The Korean Society of Propulsion Engineers
, v.10, no.4, pp.77-84,
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12 |
A Thermal Analysis of Liquid Rocket Combustors using a Modelling of Film Cooling Performance
Kim, Hong-Jip;Cho, Won-Kook;Moon, Yoon-Wan;
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The Korean Society of Propulsion Engineers
, v.10, no.4, pp.85-92,
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13 |
Film cooling Effects on Wall Heat Flux of a Subscale Calorimetric Combustion Chamber
Kim, Jong-Gyu;Lim, Byoung-Jik;Seo, Seong-Hyeon;Han, Yeoung-Min;Kim, Hong-Jip;Choi, Hwan-Seok;
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The Korean Society of Propulsion Engineers
, v.10, no.4, pp.93-99,
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14 |
Study on Installed Performance Simulation of Aircraft Gas-Turbine Engine Considering Inlet and Exhaust Losses
Kong, Chang-Duk;Owino, George.Omollo.;
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The Korean Society of Propulsion Engineers
, v.10, no.4, pp.100-108,
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