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CALLISTO reusable vehicle system design

Desmariaux, Jean and Cliquet Moreno, Elisa and Chavagnac, Christophe and Tatiossian, Pascal and Saito, Yasuhiro and Dumont, Etienne (2019) CALLISTO reusable vehicle system design. 32nd ISTS and NSAT, 15-21 June 2019, Fukui, Japan.

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Official URL: https://archive.ists.or.jp/upload_pdf/2019-g-02.pdf


JAXA, CNES, and DLR have jointly conducted concept design and project definition activities for a vertical-take off, vertical landing, experimental vehicle called CALLISTO (Cooperative Action Leading to Launcher Innovation for Stage Toss-back Operations), which objectives are to master key technologies to recover and reuse future operational reusable first stages. The vehicle has a diameter of 1.1m, it is roughly 13m high, with a mass at lift-off of roughly 3.5 tons. Main propulsion is based on LOx/LH2 RSR2 engine (enhanced version of RSR engine of JAXA RV-X experiment) and roll control system uses H2O2. This paper presents a further overview of the CALLISTO vehicle system & mission design. First, mission design is addressed, with emphasis on flight profiles and flight sequence definition. Specific technical challenges associated to each flight phase are detailed, in particular with respect to their impact on vehicle design requirements. Then vehicle design is presented, going through the main system level functional architectures. Main features are connected to mission design such as to highlight the vehicle design drivers. Finally insight into test plan is provided, which will contribute to demonstration flights de-risking logic.

Item URL in elib:https://elib.dlr.de/132889/
Document Type:Conference or Workshop Item (Speech)
Title:CALLISTO reusable vehicle system design
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Cliquet Moreno, ElisaCNESUNSPECIFIED
Chavagnac, ChristopheCNESUNSPECIFIED
Dumont, EtienneEtienne.Dumont (at) dlr.dehttps://orcid.org/0000-0003-4618-0572
Date:21 June 2019
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In ISI Web of Science:No
Keywords:CALLISTO, reusability, RLV, VTVL, toss-back, vertical take-off, vertical landing demonstrator, boostback
Event Title:32nd ISTS and NSAT
Event Location:Fukui, Japan
Event Type:international Conference
Event Dates:15-21 June 2019
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: Bremen
Institutes and Institutions:Institute of Space Systems > Systems Engineering and Project Office
Deposited By: Dumont, Etienne
Deposited On:17 Dec 2019 13:09
Last Modified:19 Aug 2021 12:05

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