session 7

Title: Hypersonic Air-breathing and Combined Cycle Propulsion, and Hypersonic Vehicle
type: oral
Description: This session covers hypersonic air-breathing and combined cycle propulsion with space applications. The typical types of engine considered in this session include: turbojet, ramjet, Scramjet, detonation engine, Turbine Based Combined Cycle (TBCC), Rocket Based Combined Cycle (RBCC), Hypersonic Pre-cooled Propulsion, Air Turbo Rocket (ATR) and other types of hypersonic combined cycle propulsion, together with the associated vehicle.
Date: 2026-10-08
Time: 10:15
Room: E6

IPC members

Co-Chair: Dr. Mario Kobald, HyImpulse Technologies GmbH, Germany;
Co-Chair: Prof. Riheng Zheng, Beihang University, China;
Rapporteur: Dr. Angelo Cervone, Delft University of Technology (TU Delft), Netherlands (Kingdom of the);

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	Dynamic Shock Shield Design and Theoretical Framework for Adaptive Spacecraft Protection during Exoplanetary Atmospheric Entry	10	confirmed	Ms. Malath Abdullah Nouh Al Alsadi		Saudi Arabia
2	10:25	State-Constrained Aeropropulsive Control for Engine-Safe Operation of Air-Breathing Hypersonic Vehicles	10	confirmed	Mr. Fatma Nur AY	Samsun University	Türkiye
3	10:35	Enhancement of Supersonic Hydrogen Combustion via Micro-Structured Lower Wall in a Scramjet Combustor	10	confirmed	Dr. Maher Dhahri	Elisa Aerospace	France
4	10:45	Sensitivity Analysis of Ramjet Inlet Pressure Recovery and Transition Behavior in a Rocket-Based Combined Cycle Engine.	10	confirmed	Ms. Ines Romdhani	Koc University	Türkiye
5	10:55	Feasibility of Rotating Detonation Engines Operated with Particulate Aluminium and Oxygen Mixtures	10	confirmed	Mr. Guillaume Knight	RMIT University	Australia
6	11:05	LES Investigation of Base Flow and Drag Characteristics of a Hypersonic Vehicle with Hot and Cold Jet Exhausts	10	confirmed	Mr. Mert Ali Yoldaş	Samsun University	Türkiye
7	11:15	flame characteristics and prediction of CH* radicals in a supersonic combustor with strut/cavity flameholders	10	confirmed	Mr. Yi Gao	Northwestern Polytechnical University	China
8	11:25	Physics-Informed Robustness Assessment of a Mach 6 Scramjet Inlet Under Geometric Uncertainty Effects	10	confirmed	Mr. Mert Emir Avci	TED University, Mechanical Engineering Department	Türkiye
9	11:35	Theoretical Analysis and Performance Evaluation of Powder-Fueled Rotating Detonation Ramjet Engines	10	confirmed	Mr. Jiebo Zhang	Beihang University (BUAA)	China
10	11:45	Crossbow’s test campaign at DLR Lampoldshausen: firing FAST Aerospace’s proprietary ramjet engine combustor demonstrator, part of the HyperDart airlaunch program	10	confirmed	Mr. Alessandro Castelvetri	FAST Aerospace Srl	Italy
11	11:55	Thrust Control System of an Air-Turbo Engine for Vertical Take-off and Landing Demonstrator Vehicle	10	confirmed	Dr. Shinichiro Tokudome	Japan Aerospace Exploration Agency (JAXA), ISAS	Japan
12	12:05	Shock tube/laser experiments to study pyrolysis and burning of airbreathing hybrid propellants	10	confirmed	Prof. Subith Vasu	University of Central Florida (UCF)	United States

session 7

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