session 5

Title: Technologies for Future Space Transportation Systems
type: oral
Description: Discussion of technologies enabling new reusable or expendable launch vehicles and in-space transportation systems. Emphasis is on early TRL hardware development and verification prior to flight, including ground testing and/or innovative technology prototype demonstrations not yet involving flight.
Date: 2024-10-16
Time: 15:00
Room: White Hall 2

IPC members

Co-Chair: Prof. Xiaowei WANG, China Academy of Launch Vehicle Technology (CALT), China;
Co-Chair: Mr. Franck Koebel, ArianeGroup, France;
Rapporteur: Ms. Shana Diez, SpaceX, United States;
Rapporteur: Mr. Christophe Bonnal, European Conference for Aero-Space Sciences (EUCASS), France;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	15:00	CRYSALIS – The Initial Design of a European Cryogenic Storage and Refuelling In-orbit Demonstrator	15	confirmed	Ms. Kathleen Blyth	Absolut System	France
2	15:15	Advancements in Qualifying the Reusable Thermal Protection System and Hot Structures of ESA Space Rider	15	confirmed	Dr. Giuseppe Rufolo	CIRA Italian Aerospace Research Centre	Italy
3	15:30	A Novel Laser Propulsion System for Microsatellite Launch	12	confirmed	Ms. Rong Chen	China Academy of Launch Vehicle Technology (CALT)	China
4	15:42	The road to HyperDart, FAST Aerospace’s partially reusable proprietary hypersonic stratolauncher for smallsat LEO delivery	12	confirmed	Mr. Alessandro Castelvetri	Politecnico di Milano	Italy
5	15:54	A Weakly Model Dependent Control Scheme for a Class of Large-Scale Long-Range Aerospace Transportation Vehicle	12	confirmed	Dr. Feng Zhang	China Academy of Launch Vehicle Technology(CALT)	China
6	16:06	Performance Improvement of Reusable SSTO with Air-Addition System	12	confirmed	Dr. Tadayoshi Shoyama	Innovative Space Carrier Inc.	Japan
7	16:18	Adaptive Augmented Control \\ for a Launch Vehicle with Fuel-Slosh	12	withdrawn	Ms. Alessia Nerattini	Sapienza University of Rome	Italy
8	16:30	Genetic Programming Guidance for the Reentry Trajectory of the ReFEx Vehicle	12	confirmed	Dr. Francesco Marchetti	German Aerospace Center (DLR), Bremen	Germany
9	16:42	European Autonomous Flight Termination Systems based in Smart Avionics	12	confirmed	Mr. Sergio Ramírez Navidad	SENER	Spain
10	16:54	Design and Development of a Modular Avionics Suite for a UK Micro-Launcher.	12	confirmed	Dr. Alexander Erlank	Orbital Express Launch Limited (Orbex)	United Kingdom
11	17:06	A downgraded trajectory optimization method combining deep neural networks and lossless convex optimization for the thrust descent failure	12	confirmed	Mr. Zongzhan Ma	Northwestern Polytechnical University，NPU	China
12	17:18	Generic flight termination architecture for launchers- Tailoring the design based on flight-proven building blocks	12	confirmed	Mr. Florian THIVENT	PYROALLIANCE	France

session 5

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