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CALLISTO: A Prototype Paving the Way for Reusable Launch Vehicles in Europe and Japan

Dumont, Etienne and Illig, Michel and Ishimoto, Shinji and Chavagnac, Christophe and Saito, Yasuhiro and Krummen, Sven and Eichel, Silas and Martens, Hauke and Giagkozoglou, Sofia and Häseker, Janis Sebastian and Ecker, Tobias and Klevanski, Josef and Krziwanie, Felix and Rotärmel, Waldemar and Schröder, Silvio and Schneider, Anton and Grimm, Christian and Woicke, Svenja and Sagliano, Marco and Schlotterer, Markus and Markgraf, Markus and Braun, Benjamin and Aicher, Moritz and Briese, Lale Evrim and Petkov, Ivaylo and Riehmer, Johannes and Reimann, Bodo (2022) CALLISTO: A Prototype Paving the Way for Reusable Launch Vehicles in Europe and Japan. 73rd International Astronautical Congress (IAC), 2022-09-18 - 2022-09-22, Paris, Frankreich.

Full text not available from this repository.

Abstract

Japan and Europe are getting ready for the maiden flight of their new workhorse launch vehicles: H-3 and Ariane 6. While both vehicles are following an expendable design, reusable vertical take-off and vertical landing (VTVL) concepts are successfully tested and operated in the USA. This evolution has shown that reusability can be a solution for further improvement of competitiveness, versatility and sustainability of future launch system. In order to understand the specificities of reusable launch vehicles in terms of design, optimization and operations, and mature the required key technologies, CNES, DLR and JAXA have decided to join their competences in the project CALLISTO (Cooperative Action Leading to Launcher Innovation in Stage Toss - back Operations). The project aims at developing, building and testing a prototype vehicle which shall, without a technological precursor, demonstrate the mastering of flights and operations representative to a reusable launcher stage. Along all project phases, data and knowhow are being gained about design, manufacturing, operations and maintenance solutions, which are essential for the development of future operational vehicles. CALLISTO vehicle is about 13 m high and 1.1 m diameter, propelled by a JAXA LOX/LH2 engine able to reignite in flight and with continuous deep throttling capability. It is equipped with deployable landing legs and aerodynamic control surfaces. It will be operated from the Diamant launch pad at the French Guiana Space Centre and sized for about 10 flights following different mission profiles, opening the flight domain from low altitude test up to domain relevant for operational vehicles. This paper intends to give an overview about the current status of the project and especially the development status of the aerodynamic analyses, of selected products of the vehicle and of the ground segment.

Item URL in elib:https://elib.dlr.de/188663/
Document Type:Conference or Workshop Item (Speech)
Title:CALLISTO: A Prototype Paving the Way for Reusable Launch Vehicles in Europe and Japan
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Dumont, EtienneUNSPECIFIEDhttps://orcid.org/0000-0003-4618-0572UNSPECIFIED
Illig, MichelCNESUNSPECIFIEDUNSPECIFIED
Ishimoto, ShinjiJAXAUNSPECIFIEDUNSPECIFIED
Chavagnac, ChristopheCNESUNSPECIFIEDUNSPECIFIED
Saito, YasuhiroJAXAUNSPECIFIEDUNSPECIFIED
Krummen, SvenUNSPECIFIEDhttps://orcid.org/0000-0002-4126-688XUNSPECIFIED
Eichel, SilasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Martens, HaukeUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Giagkozoglou, SofiaUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Häseker, Janis SebastianUNSPECIFIEDhttps://orcid.org/0000-0003-1187-5972UNSPECIFIED
Ecker, TobiasUNSPECIFIEDhttps://orcid.org/0000-0001-7134-1185UNSPECIFIED
Klevanski, JosefUNSPECIFIEDhttps://orcid.org/0009-0002-4336-1116UNSPECIFIED
Krziwanie, FelixUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Rotärmel, WaldemarUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Schröder, SilvioUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Schneider, AntonUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Grimm, ChristianUNSPECIFIEDhttps://orcid.org/0000-0003-4490-7424UNSPECIFIED
Woicke, SvenjaUNSPECIFIEDhttps://orcid.org/0000-0002-0864-9977UNSPECIFIED
Sagliano, MarcoUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Schlotterer, MarkusUNSPECIFIEDhttps://orcid.org/0000-0002-6565-3622UNSPECIFIED
Markgraf, MarkusUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Braun, BenjaminUNSPECIFIEDhttps://orcid.org/0000-0002-0193-6607UNSPECIFIED
Aicher, MoritzUNSPECIFIEDhttps://orcid.org/0000-0002-2150-713XUNSPECIFIED
Briese, Lale EvrimUNSPECIFIEDhttps://orcid.org/0000-0003-0900-2005UNSPECIFIED
Petkov, IvayloUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Riehmer, JohannesUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Reimann, BodoUNSPECIFIEDhttps://orcid.org/0000-0001-7765-7295UNSPECIFIED
Date:21 September 2022
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:CALLISTO, Reusability, Demonstrator, RLV, VTVL, CSG
Event Title:73rd International Astronautical Congress (IAC)
Event Location:Paris, Frankreich
Event Type:international Conference
Event Start Date:18 September 2022
Event End Date:22 September 2022
Organizer:IAF
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Project CALLISTO [RP]
Location: Braunschweig , Bremen , Göttingen , Köln-Porz , Oberpfaffenhofen , Stuttgart
Institutes and Institutions:Institute of Space Systems > Systems Engineering and Project Office
Institute of Structures and Design > Space System Integration
Institute of Space Systems > Quality Management and Product Assurance for Space Systems
Institute of Space Systems > Avionics Systems
Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Institute for Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology
Institute of Space Systems > Land and Exploration Technology
Institute of Space Systems > Navigation and Control Systems
Space Operations and Astronaut Training > Space Flight Technology
Institute of System Dynamics and Control > Space System Dynamics
Institute for Aerodynamics and Flow Technology > Spacecraft, BS
Deposited By: Dumont, Etienne
Deposited On:06 Oct 2022 10:01
Last Modified:24 Apr 2024 20:49

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