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Thermal characterizations of the paraffin wax/low density polyethylene blends as a solid fuel

Thermochimica acta, 2015-08, Vol.613, p.9-16

2015

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The Effect of the Rotating Disk Geometry on the Flow and Flux Enhancement in a Dynamic Filtration System

Membranes (Basel), 2023-02, Vol.13 (3), p.291

2023

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Experimental investigation of the effects of paraffin/aluminum blended fuels on aluminum particle size

Journal of Mechanical Science and Technology, 2019, 33(6), , pp.3011-3018

2019

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Morphological classification of disintegration behavior of viscoelastic simulant gel propellant in coaxial streams

Journal of visualization, 2020-04, Vol.23 (2), p.287-298

2020

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Development of 200 N-class throttleable hybrid rocket motor for lunar module application

FirePhysChem (Online), 2021-12, Vol.1 (4), p.251-259

2021

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Thermal–Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing

Journal of propulsion and power, 2023-05, Vol.39 (3), p.308-317

2023

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Combustion Instability Mechanism in Hybrid Rocket Motors with Diaphragm

Journal of propulsion and power, 2022-03, Vol.38 (2), p.309-318

2022

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Evaluation of Paraffin–Polyethylene Blends as Novel Solid Fuel for Hybrid Rockets

Journal of propulsion and power, 2015-11, Vol.31 (6), p.1750-1760

2015

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Flow visualization of cryogenic spray from a movable pintle injector

Journal of visualization, 2019-08, Vol.22 (4), p.773-781

2019

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Role of axial mass and strange axial form factor from various target nuclei in neutrino-nucleus scattering

Physical review. C, 2019-09, Vol.100 (3), Article 034604

2019

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Study on Spray Characteristics of Simulant Gel in Pressure Swirl Injector

International Journal of Aeronautical and Space Sciences, 2022, 23(4), , pp.794-803

2022

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Hybrid Rocket Underwater Propulsion: A Preliminary Assessment

Aerospace, 2019-03, Vol.6 (3), p.28

2019

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Mass Transfer Number Sensitivity on the Fuel Burning Rate in Hybrid Rockets

Journal of propulsion and power, 2015-07, Vol.31 (4), p.1041-1050

2015

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Regression Characteristics of the Cylindrical Multiport Grain in Hybrid Rockets

Journal of propulsion and power, 2013-05, Vol.29 (3), p.573-581

2013

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Effect of pintle on the acoustic field and stability factors of a solid-propellant rocket motor with variable pintle thruster

Journal of Mechanical Science and Technology, 2015, 29(3), , pp.923-929

2015

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Experimental Investigation on Combustion Characteristics of Liquid Kerosene and Gelled Kerosene Using Shear Coaxial Injector

Journal of the Korean Society of Propulsion Engineers, 2020-06, Vol.24 (3), p.1-11

2020

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Internal Ballistics Analysis and Experimental Validation of Thrust Modulation for Hybrid Rocket Using Self-Pressurizing Nitrous Oxide

Journal of the Korean Society of Propulsion Engineers, 2020-06, Vol.24 (3), p.47-58

2020

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Evaluation of Nozzle’s Combustion Instability Suppression Effect by Linearized Euler Equation

Journal of the Korean Society of Propulsion Engineers, 2019-12, Vol.23 (6), p.1-10

2019

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Study on Breakup Characteristics of Gel Propellant Using Pressure Swirl Injector

Journal of the Korean Society of Propulsion Engineers, 2021-10, Vol.25 (5), p.10-17

2021

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A Study on the Combustion Characteristics of Paraffin Fuel Based Hybrid Rocket with the Post Chamber L/D Ratio

Journal of the Korean Society of Propulsion Engineers, 2019-10, Vol.23 (5), p.19-26

2019

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Flow Characteristics Investigation of Gel Propellant with Al 2 O 3 Nano Particles in a Curved Duct Channel

Journal of the Korean Society of Propulsion Engineers, 2013-06, Vol.17 (3), p.47-55

2013

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Thermal and Rheological Characteristics of Paraffin Based Fuel on Aluminum Particle Size for Hybrid Rocket Application

Journal of the Korean Society of Propulsion Engineers, 2018-04, Vol.22 (2), p.108-114

2018

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Surface Tension Change of Simulant Gel Propellant according to the Metal Particle Addition

Journal of the Korean Society of Propulsion Engineers, 2017-06, Vol.21 (3), p.34-40

2017

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Trade-off Evaluation due to Application of Mixing Chamber for Hybrid Rocket-Propulsion System

Journal of Aerospace System Engineering, 2016-09, Vol.10 (3), p.23-31

2016

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Rheological Investigation of Aluminized Paraffin Wax Fuel on Particle Size and Contents

Journal of the Korean Society of Propulsion Engineers, 2018-04, Vol.22 (2), p.11-19

2018

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Thermal characterizations of the paraffin wax/low density polyethylene blends as a solid fuel

The Effect of the Rotating Disk Geometry on the Flow and Flux Enhancement in a Dynamic Filtration System

Experimental investigation of the effects of paraffin/aluminum blended fuels on aluminum particle size

Morphological classification of disintegration behavior of viscoelastic simulant gel propellant in coaxial streams

Development of 200 N-class throttleable hybrid rocket motor for lunar module application

Thermal–Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing

Combustion Instability Mechanism in Hybrid Rocket Motors with Diaphragm

Evaluation of Paraffin–Polyethylene Blends as Novel Solid Fuel for Hybrid Rockets

Flow visualization of cryogenic spray from a movable pintle injector

Role of axial mass and strange axial form factor from various target nuclei in neutrino-nucleus scattering

Study on Spray Characteristics of Simulant Gel in Pressure Swirl Injector

Hybrid Rocket Underwater Propulsion: A Preliminary Assessment

Mass Transfer Number Sensitivity on the Fuel Burning Rate in Hybrid Rockets

Regression Characteristics of the Cylindrical Multiport Grain in Hybrid Rockets

Effect of pintle on the acoustic field and stability factors of a solid-propellant rocket motor with variable pintle thruster

Experimental Investigation on Combustion Characteristics of Liquid Kerosene and Gelled Kerosene Using Shear Coaxial Injector

Internal Ballistics Analysis and Experimental Validation of Thrust Modulation for Hybrid Rocket Using Self-Pressurizing Nitrous Oxide

Evaluation of Nozzle’s Combustion Instability Suppression Effect by Linearized Euler Equation

Study on Breakup Characteristics of Gel Propellant Using Pressure Swirl Injector

A Study on the Combustion Characteristics of Paraffin Fuel Based Hybrid Rocket with the Post Chamber L/D Ratio

Flow Characteristics Investigation of Gel Propellant with Al 2 O 3 Nano Particles in a Curved Duct Channel

Thermal and Rheological Characteristics of Paraffin Based Fuel on Aluminum Particle Size for Hybrid Rocket Application

Surface Tension Change of Simulant Gel Propellant according to the Metal Particle Addition

Trade-off Evaluation due to Application of Mixing Chamber for Hybrid Rocket-Propulsion System

Rheological Investigation of Aluminized Paraffin Wax Fuel on Particle Size and Contents

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