Category Archives: Propulsion Systems and Components

The Red Kite Sounding Rocket Motor Qualification Milestones and Application Spectrum

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-Prus June 7, 2024

F. SCHEUERPFLUG, T. RÖHR, T. HUBER, M. REINOLD, D. HARGARTEN, L. KOBOW, R. KIRCHHARTZ, M. KUHN, A. Weigand, M. BERNDL, J. WERNETH

DOI Number: https://doi.org/10.82241/ceas-hisst-2024-368

Conference number: HiSST-2024-368

Numerical Study on the Characteristics of Detonation Wave Number in RDE

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-Prus June 7, 2024

Mohammed N. NEJAAMTHEEN, Bu-Kyeng SUNG, Jeong-Yeol CHOI

DOI Number: https://doi.org/10.82241/ceas-hisst-2024-352

Conference number: HiSST-2024-352

Numerical Investigation on the Flow Dynamics of Interaction between Two Liquid-liquid Bi-swirl Injectors

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-Prus June 7, 2024

Vishnu NATARAJAN, Jongsu OH, Jeong-Yeol CHOI

DOI Number: https://doi.org/10.82241/ceas-hisst-2024-351

Conference number: HiSST-2024-351

Numerical Study of Reactive Flow dynamics in a Hydrogen-fueled Direct-Connect Scramjet Combustor depending on Number of Injector

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-Prus June 7, 2024

Seung-Min JEONG, Jae-Eun KIM, Jeong-Yeol CHOI

DOI Number: https://doi.org/10.82241/ceas-hisst-2024-350

Conference number: HiSST-2024-350

Spray Characteristics of High Energetic Powder Added Low-Temperature Gel Fuel using Pressure Swirl Injector

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-Prus June 7, 2024

Dong-Geun LEE, Sul-Hee KIM, In-Woong LEE, Dong-Hee LEE, Hee-Jang MOON

DOI Number: N/A

Conference number: HiSST-2024-349

A Numerical Simulation on the Unsteady Flow in a GCH4-GOx Small Thrust Chamber

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-Prus June 7, 2024

Hong Yeong PARK, Yun Hyeong KANG, Chang Han BAE, Jeong Soo KIM

DOI Number: https://doi.org/10.82241/ceas-hisst-2024-341

Conference number: HiSST-2024-341

Nitrogen Oxides Emission Estimation for a Hydrogen-fuelled Dual-Mode Ramjet in the Conceptual Design Phase

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-Prus June 6, 2024

Valeria BORIO, Roberta FUSARO, Nicole VIOLA, Guido SACCONE2,Ginevra CIANCI

DOI Number: https://doi.org/10.82241/ceas-hisst-2024-334

Conference number: HiSST-2024-334

IDDES Modeling of a Dual-mode Scramjet by Dynamic Zone Flamelet Model with Sensitivity Analysis of Zoning Parameter

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-Prus June 6, 2024

Zheng ZHANG, Wei YAO

DOI Number: N/A

Conference paper: HiSST-2024-333

Thrust Enhancement of Rocket-Deployed Dual-Mode Ramjet Engine

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-Prus June 6, 2024

Sangwook JIN, Haeseung JEONG, Minchan KWON, Juhyun BAE, Seokjin OH, Hojin CHOI, Jaehoon RYU, Suji LEE

DOI Number: https://doi.org/10.82241/ceas-hisst-2024-331

Conference number: HiSST-2024-331

Numerical Study of Turbulent Combustion in High Mach Number Scramjet Engine with Thermodynamic Non-equilibrium Effect

1.Events, HiSST 2024, Propulsion Systems and ComponentsBy Beata Wierzbińska-Prus June 6, 2024

Hai FENG, Tai JIN, Kun WU

DOI Number: N/A

Conference number: HiSST-2024-328