MAIUS-1 - Vehicle, Subsystems Design and Mission Operations

In November 2015, the DLR Mobile Rocket Base will launch the MAIUS-1 rocket vehicle at Esrange, Northern Sweden. The MAIUS-A experiment is a pathfinder atom optics experiment. The scientific objective of the mission is the first creation of a Bose-Einstein Condensate in space and performing atom int...

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Main Authors: Stamminger, Andreas, Ettl, Josef, Grosse, Jens, Hörschgen-Eggers, Marcus, Jung, Wolfgang, Kallenbach, Alexander, Raith, Georg, Saedtler, Wolfram, Seidel, Stephan, Turner, John, Wittkamp, Markus
Format: Conference Object
Language:German
Published: ESA Communications 2015
Subjects:
Online Access:https://elib.dlr.de/99281/
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author Stamminger, Andreas
Ettl, Josef
Grosse, Jens
Hörschgen-Eggers, Marcus
Jung, Wolfgang
Kallenbach, Alexander
Raith, Georg
Saedtler, Wolfram
Seidel, Stephan
Turner, John
Wittkamp, Markus
author_facet Stamminger, Andreas
Ettl, Josef
Grosse, Jens
Hörschgen-Eggers, Marcus
Jung, Wolfgang
Kallenbach, Alexander
Raith, Georg
Saedtler, Wolfram
Seidel, Stephan
Turner, John
Wittkamp, Markus
author_sort Stamminger, Andreas
collection Unknown
description In November 2015, the DLR Mobile Rocket Base will launch the MAIUS-1 rocket vehicle at Esrange, Northern Sweden. The MAIUS-A experiment is a pathfinder atom optics experiment. The scientific objective of the mission is the first creation of a Bose-Einstein Condensate in space and performing atom interferometry on a sounding rocket. MAIUS-1 comprises a two-stage unguided solid propellant VSB-30 rocket motor system. The vehicle consists of a Brazilian S31 motor as 1st stage, a S30 motor as 2nd stage, a conical motor adapter, a despin module, a payload adapter, the MAIUS-A experiment consisting of five experiment modules, an attitude control system module, a newly developed conical service system, and a two-staged recovery system including a nosecone. In contrast to usual payloads on VSB-30 rockets, the payload has a diameter of 500 mm due to constraints of the scientific experiment. Because of this change in design, a blunted nosecone is necessary to guarantee the required static stability during the ascent phase of the flight. This paper will give an overview on the subsystems which have been built at DLR MORABA, especially the newly developed service system. Further, it will contain a description of the MAIUS-1 vehicle, the mission and the unique requirements on operations and attitude control, which is additionally required to achieve a required attitude with respect to the nadir vector. Additionally to a usual microgravity environment, the MAIUS-1 payload requires attitude control to achieve a required attitude with respect to the nadir vector.
format Conference Object
genre Northern Sweden
genre_facet Northern Sweden
geographic Esrange
geographic_facet Esrange
id ftdlr:oai:elib.dlr.de:99281
institution Open Polar
language German
long_lat ENVELOPE(21.117,21.117,67.883,67.883)
op_collection_id ftdlr
op_relation https://elib.dlr.de/99281/1/2015-07-04%20Stamminger%20-%20MAIUS-1.pdf
Stamminger, Andreas und Ettl, Josef und Grosse, Jens und Hörschgen-Eggers, Marcus und Jung, Wolfgang und Kallenbach, Alexander und Raith, Georg und Saedtler, Wolfram und Seidel, Stephan und Turner, John und Wittkamp, Markus (2015) MAIUS-1 - Vehicle, Subsystems Design and Mission Operations. In: Proceedings 22nd ESA Symposium on European Rocket and Balloon Programmes and Related Research, SP-730, Seiten 183-190. ESA Communications. 22nd ESA Symposium on European Rocket and Balloon Programmes and Related Research, 2015-06-07 - 2015-06-12, Tromsø, Norwegen. ISBN 978-92-9221-294-0. ISSN 1609-042CX.
publishDate 2015
publisher ESA Communications
record_format openpolar
spelling ftdlr:oai:elib.dlr.de:99281 2025-06-15T14:44:31+00:00 MAIUS-1 - Vehicle, Subsystems Design and Mission Operations Stamminger, Andreas Ettl, Josef Grosse, Jens Hörschgen-Eggers, Marcus Jung, Wolfgang Kallenbach, Alexander Raith, Georg Saedtler, Wolfram Seidel, Stephan Turner, John Wittkamp, Markus 2015-09 application/pdf https://elib.dlr.de/99281/ de ger ESA Communications https://elib.dlr.de/99281/1/2015-07-04%20Stamminger%20-%20MAIUS-1.pdf Stamminger, Andreas und Ettl, Josef und Grosse, Jens und Hörschgen-Eggers, Marcus und Jung, Wolfgang und Kallenbach, Alexander und Raith, Georg und Saedtler, Wolfram und Seidel, Stephan und Turner, John und Wittkamp, Markus (2015) MAIUS-1 - Vehicle, Subsystems Design and Mission Operations. In: Proceedings 22nd ESA Symposium on European Rocket and Balloon Programmes and Related Research, SP-730, Seiten 183-190. ESA Communications. 22nd ESA Symposium on European Rocket and Balloon Programmes and Related Research, 2015-06-07 - 2015-06-12, Tromsø, Norwegen. ISBN 978-92-9221-294-0. ISSN 1609-042CX. Mobile Raketenbasis Institut für Raumfahrtsysteme Konferenzbeitrag NonPeerReviewed 2015 ftdlr 2025-06-04T04:58:07Z In November 2015, the DLR Mobile Rocket Base will launch the MAIUS-1 rocket vehicle at Esrange, Northern Sweden. The MAIUS-A experiment is a pathfinder atom optics experiment. The scientific objective of the mission is the first creation of a Bose-Einstein Condensate in space and performing atom interferometry on a sounding rocket. MAIUS-1 comprises a two-stage unguided solid propellant VSB-30 rocket motor system. The vehicle consists of a Brazilian S31 motor as 1st stage, a S30 motor as 2nd stage, a conical motor adapter, a despin module, a payload adapter, the MAIUS-A experiment consisting of five experiment modules, an attitude control system module, a newly developed conical service system, and a two-staged recovery system including a nosecone. In contrast to usual payloads on VSB-30 rockets, the payload has a diameter of 500 mm due to constraints of the scientific experiment. Because of this change in design, a blunted nosecone is necessary to guarantee the required static stability during the ascent phase of the flight. This paper will give an overview on the subsystems which have been built at DLR MORABA, especially the newly developed service system. Further, it will contain a description of the MAIUS-1 vehicle, the mission and the unique requirements on operations and attitude control, which is additionally required to achieve a required attitude with respect to the nadir vector. Additionally to a usual microgravity environment, the MAIUS-1 payload requires attitude control to achieve a required attitude with respect to the nadir vector. Conference Object Northern Sweden Unknown Esrange ENVELOPE(21.117,21.117,67.883,67.883)
spellingShingle Mobile Raketenbasis
Institut für Raumfahrtsysteme
Stamminger, Andreas
Ettl, Josef
Grosse, Jens
Hörschgen-Eggers, Marcus
Jung, Wolfgang
Kallenbach, Alexander
Raith, Georg
Saedtler, Wolfram
Seidel, Stephan
Turner, John
Wittkamp, Markus
MAIUS-1 - Vehicle, Subsystems Design and Mission Operations
title MAIUS-1 - Vehicle, Subsystems Design and Mission Operations
title_full MAIUS-1 - Vehicle, Subsystems Design and Mission Operations
title_fullStr MAIUS-1 - Vehicle, Subsystems Design and Mission Operations
title_full_unstemmed MAIUS-1 - Vehicle, Subsystems Design and Mission Operations
title_short MAIUS-1 - Vehicle, Subsystems Design and Mission Operations
title_sort maius-1 - vehicle, subsystems design and mission operations
topic Mobile Raketenbasis
Institut für Raumfahrtsysteme
topic_facet Mobile Raketenbasis
Institut für Raumfahrtsysteme
url https://elib.dlr.de/99281/