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The SQUID sounding rocket experiment
KTH, School of Engineering Sciences (SCI), Mechanics, Structural Mechanics.
KTH, School of Engineering Sciences (SCI), Mechanics, Structural Mechanics.
KTH, School of Engineering Sciences (SCI), Mechanics, Structural Mechanics.
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2011 (English)In: Proceedings of the 20th ESA Symposium on European Rocket and Balloon Programmes and Related Research, European Space Agency, 2011, p. 159-166Conference paper, Published paper (Refereed)
Abstract [en]

The objective of the SQUID project is to develop and in flight verify a miniature version of a wire boom deployment mechanism to be used for electric field measurements in the ionosphere. In February 2011 a small ejectable payload, built by a team of students from The Royal Institute of Technology (KTH), was launched from Esrange on-board the REXUS-10 sounding rocket. The payload separated from the rocket, deployed and retracted the wire booms, landed with a parachute and was subsequently recovered. Here the design of the experiment and post fight analysis are presented.

Place, publisher, year, edition, pages
European Space Agency, 2011. p. 159-166
Series
ESA Special Publications, ISSN 0379-6566 ; 700
National Category
Aerospace Engineering Applied Mechanics Communication Systems Fusion, Plasma and Space Physics
Identifiers
URN: urn:nbn:se:kth:diva-85604ISI: 000324759000022Scopus ID: 2-s2.0-84859906978ISBN: 978-92-9092-264-3 (print)OAI: oai:DiVA.org:kth-85604DiVA, id: diva2:500080
Conference
20th ESA Symposium on European Rocket and Balloon Programmes and Related Research, Hyères, France, 22-26 May 2011
Note

QC 20120411

Available from: 2012-02-13 Created: 2012-02-13 Last updated: 2022-06-24Bibliographically approved

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Ivchenko, NickolayTibert, Gunnar

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CiteExportLink to record
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Citation style
  • apa
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
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Language
  • de-DE
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  • nn-NO
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Output format
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