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Prototype of an ultra-stable optic cavity for space applications

hal.structure.identifierSystèmes de Référence Temps Espace [SYRTE]
dc.contributor.authorARGENCE, Bérengère
hal.structure.identifierSODERN
dc.contributor.authorPREVOST, Eddie
hal.structure.identifierCentre National d'Études Spatiales [Toulouse] [CNES]
dc.contributor.authorLÉVÈQUE, Thomas
hal.structure.identifierSODERN
dc.contributor.authorLE GOFF, Roland
hal.structure.identifierSystèmes de Référence Temps Espace [SYRTE]
dc.contributor.authorLEMONDE, Pierre
hal.structure.identifierSystèmes de Référence Temps Espace [SYRTE]
dc.contributor.authorBIZE, Sebastien
hal.structure.identifierlp2n-06,lp2n-14
hal.structure.identifierSystèmes de Référence Temps Espace [SYRTE]
dc.contributor.authorSANTARELLI, Giorgio
dc.date.accessioned2023-05-12T10:23:57Z
dc.date.available2023-05-12T10:23:57Z
dc.date.issued2012-10-25
dc.identifier.issn1094-4087
dc.identifier.urihttps://oskar-bordeaux.fr/handle/20.500.12278/181199
dc.description.abstractEnWe report the main features and performances of a prototype of an ultra-stable cavity designed and realized by industry for space applications with the aim of space missions. The cavity is a 100 mm long cylinder rigidly held at its midplane by a engineered mechanical interface providing an efficient decoupling from thermal and vibration perturbations. Intensive finite element modeling was performed in order to optimize thermal and vibration sensitivities while getting a high fundamental resonance frequency. The system was designed to be transportable, acceleration tolerant (up to several g) and temperature range compliant [−33◦C;73◦C]. Thermal isolation is ensured by gold coated Aluminum shields inside a stainless steel enclosure for vacuum. The axial vibration sensitivity was evaluated at(4±0.5)×10 −11/(m.s−2), while the transverse one is <1×10−11/(m.s−2). The fractional frequency instability is 1×10−15 from 0.1 to a few seconds and reaches 5−6×10−16at 1s.
dc.language.isoen
dc.publisherOptical Society of America - OSA Publishing
dc.title.enPrototype of an ultra-stable optic cavity for space applications
dc.typeArticle de revue
dc.identifier.doi10.1364/OE.20.025409
dc.subject.halPhysique [physics]/Physique [physics]/Optique [physics.optics]
dc.subject.halPhysique [physics]
dc.subject.halPhysique [physics]/Astrophysique [astro-ph]
bordeaux.journalOptics Express
bordeaux.page25409-25420
bordeaux.volume20
bordeaux.hal.laboratoriesLaboratoire Photonique, Numérique et Nanosciences (LP2N) - UMR 5298*
bordeaux.issue23
bordeaux.institutionUniversité de Bordeaux
bordeaux.institutionCNRS
bordeaux.peerReviewedoui
hal.identifierhal-00813602
hal.version1
dc.subject.itMetrological instrumentation
dc.subject.itSpace instrumentation
dc.subject.itFabry-Perot
dc.subject.itLaser stabilization
dc.subject.itOptical resonators
hal.origin.linkhttps://hal.archives-ouvertes.fr//hal-00813602v1
bordeaux.COinSctx_ver=Z39.88-2004&amp;rft_val_fmt=info:ofi/fmt:kev:mtx:journal&amp;rft.jtitle=Optics%20Express&amp;rft.date=2012-10-25&amp;rft.volume=20&amp;rft.issue=23&amp;rft.spage=25409-25420&amp;rft.epage=25409-25420&amp;rft.eissn=1094-4087&amp;rft.issn=1094-4087&amp;rft.au=ARGENCE,%20B%C3%A9reng%C3%A8re&amp;PREVOST,%20Eddie&amp;L%C3%89V%C3%88QUE,%20Thomas&amp;LE%20GOFF,%20Roland&amp;LEMONDE,%20Pierre&amp;rft.genre=article


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