International Conference on Space Optics — ICSO 2010最新文献

{"title":"METIS, the Multi Element Telescope for Imaging and Spectroscopy: for the solar orbiter mission","authors":"G. Naletto, E. Antonucci, V. Andretta, E. Battistelli, S. Cesare, V. Deppo, F. D’Angelo, S. Fineschi, M. Focardi, P. Lamy, F. Landini, D. Moses, G. Nicolini, P. Nicolosi, M. Pancrazzi, M. Pelizzo, L. Poletto, M. Romoli, S. Solanki, D. Spadaro, L. Teriaca, M. Uslenghi, L. Zangrilli","doi":"10.1117/12.2553106","DOIUrl":"https://doi.org/10.1117/12.2553106","url":null,"abstract":"University of Padova – Department of Information Engineering, Via Gradenigo, 6/B, 35131 Padova, Italy; GN: naletto@dei.unipd.it, PN: nicolosi@dei.unipd.it. CNR (National Council for Research) Institute of Photonics and Nanotechnologies, Division of Padova, via Trasea 7, 35131 Padova; VdD: dadeppo@dei.unipd.it, MGP: pelizzo@dei.unipd.it, LP: poletto@dei.unipd.it INAF (National Institute for Astrophysics) – Turin Astronomical Observatory, Via dell’Osservatorio, 20 I-10025 Pino Torinese TO, Italy; EA: antonucci@oato.inaf.it, SF: fineschi@oato.inaf.it, GN: solarproj@oato.inaf.it, LZ: zangrilli@oato.inaf.it. INAF – Napoli Capodimonte Astronomical Observatory, Salita Moiariello, 16, I-80131 Napoli, Italy; andretta@oacn.inaf.it. Selex Galileo, Via Einstein, 35, I-50013 Campi Bisenzio FI, Italy; enrico.battistelli@selexgalileo.com. Thales Alenia Space, Strada Antica Di Collegno 253 Torino, Italy; SC: stefano.cesare@thalesaleniaspace.com, FdA: filippo.dangelo@thalesaleniaspace.com University of Florence – Department of Physics and Astronomy, Largo Enrico Fermi, 2, I-50125 Firenze, Italy; MF: mauro@arcetri.astro.it, FL: flandini@arcetri.astro.it, MP: panc@arcetri.astro.it, MR: marco.romoli@unifi.it. Laboratoire d'Astrophysique de Marseille, 38, rue Frederic Joliot-Curie, 13388 Marseille cedex 13, France; philippe.lamy@oamp.fr. U.S. Naval Research Laboratory, 4555 Overlook Ave., SW, Washington, DC 20375, USA; moses@nrl.navy.mil. Max Planck Institute fur Sonnensystemforschung, Max-Planck-Str. 2, D-37191 Katlenburg-Lindau, Germany; SS: solanki@linmpi.mpg.de, LT: teriaca@linmpi.mpg.de. INAF – Catania Astronomical Observatory, Via S.Sofia 78, I-95123 Catania, Italy; dspadaro@oact.inaf.it. INAF – Institute of Space Astrophysics and Cosmic Physics, Via E. Bassini 15, I-20133 Milano; Italy. uslenghi@iasf-milano.inaf.it. *Contact author.","PeriodicalId":237474,"journal":{"name":"International Conference on Space Optics — ICSO 2010","volume":"6 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-09-09","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134579645","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

{"title":"ChemCam on the next NASA mission to Mars (MSL-2011): measured performance of the high power LIBS laser beam","authors":"N. L. Roch, J. Dalmau, L. Parès","doi":"10.1117/12.2552552","DOIUrl":"https://doi.org/10.1117/12.2552552","url":null,"abstract":"ChemCam is one of the ten instruments on the Mars Science Laboratory (also called Curiosity), a big rover being built by Jet Propulsion Laboratory (JPL), for the next NASA mission to Mars (MSL 2011). ChemCam is a suite consisting of two remote sensing instruments: a Laser-Induced Breakdown Spectrometer (LIBS) [1] and a Remote Micro-Imager (RMI) [2]. LIBS provides elemental composition of rocks and soils, while the RMI places the LIBS analyses in their geomorphologic context.","PeriodicalId":237474,"journal":{"name":"International Conference on Space Optics — ICSO 2010","volume":"19 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-09-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"121488981","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

{"title":"The Brazilian multispectral camera (MUX) for the China-Brazil earth resources satellite: Cbers 3 and 4","authors":"E. G. Carvalho, L. C. N. Scaduto, A. L. Soares, A. G. Santos, S. Evangelista, D. C. Rebolho, Anderson R. Santos, L. Azeka, W. M. Souza, R. Modugno, R. Cartolano, L. F. Vales, A. Malavolta, S. Ba, Fabiano S. dos Santos, L. Candeloro, D. Segoria, J. C. C. Neto, Opto Eletrônica","doi":"10.1117/12.2552746","DOIUrl":"https://doi.org/10.1117/12.2552746","url":null,"abstract":"This paper aims to present the optical system of th e Multispectral Camera MUX that is part of the payl oad for the CBERS 3 & 4 satellite (China Brazil Earth Resources Satellite). The CBERS program was created by Brazil and China for the development of Earth remote sensi ng satellites. The MUX camera is being developed by the Brazilian company OPTO ELETRONICA S.A. and consists of a multispectral camera with four spectral bands covering the wavelength range from blue to near inf rared (from 450nm to 890nm) with a ground resolution of 20m and a ground swath width of 120 km. Besides MUX camera (optical system, signal processing electron ics and mechanical frame), this company is also develop ing the Ground Support Equipment ‐ GSE of this camera and is responsible for structural and environmental tests. At the moment, the project is in the Qualif ication Model (QM). During this phase of the development, the camera shall be submitted to several tests, incl uding environmental, optical and structural tests with th e objective of qualify the project and start the fl ight models manufacturing.","PeriodicalId":237474,"journal":{"name":"International Conference on Space Optics — ICSO 2010","volume":"47 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-09-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"114824370","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

{"title":"Electronic speckle pattern interferometry in long wave infrared: a new technique for combining temperature and displacement measurements: application in thermo-mechanical assessment of structures","authors":"M. Georges, J. Vandenrijt, C. Thizy, Y. Stockman, I. Alexeenko","doi":"10.1117/12.2552639","DOIUrl":"https://doi.org/10.1117/12.2552639","url":null,"abstract":"Holographic and speckle based techniques are well known for measuring full-field displacements and performing non destructive testing on solid objects [1]. The measurement range and accuracy of these techniques are related to the wavelength of the laser. In visible light they are often not well suited for field applications or for large displacement measurement due to the short wavelength used, which imposes high stability constraints. One way to decrease this sensitivity is to use a longer wavelength. Our purpose is to investigate holography in the Long Wave InfraRed (LWIR) range and more specifically at 10 μm with CO2 lasers. This provides a typical 20 factor of decrease of the stability requirements; meantime the range of measurement is increased by the same factor. We present here advanced results obtained within the FANTOM FP7 project. Besides the lower sensitivity to external perturbations, another interesting feature that is put forward in this project is the possibility to develop a sensor which combines displacement by holography/speckle and thermography measurements. Here we take advantage to the fact that the necessary observation device for the holographic signal is a thermographic camera. This has an interest in various applications such as analysis of thermo-mechanical behaviour of structures or non destructive testing, where often displacements and temperature fields need to be observed and correlated one to another. We already presented preliminary results on out-of-plane and in-plane ESPI at 10.6 μm, and also on digital holographic interferometry [2], however without combining thermography. Recently we presented an improved digital holographic interferometry set-up [2], and a study of the scattering problems arising when working at such long wavelengths [3]. In this paper we present for the first time to our knowledge the combination of full-field temperature and displacements, with a single sensor.","PeriodicalId":237474,"journal":{"name":"International Conference on Space Optics — ICSO 2010","volume":"9 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-09-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"124635717","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

{"title":"The Jem‐Euso mission and its challenging optics system","authors":"A. Z. Marchi, Y. Takizawa, R. Young","doi":"10.1117/12.2552564","DOIUrl":"https://doi.org/10.1117/12.2552564","url":null,"abstract":"The Extreme Universe Space Observatory (EUSO), onboard the Japanese Experiment Module (JEM) of the International Space Station (ISS), is a project led by Japan, with contributions from the United States, Italy, Germany, France, Spain, Switzerland, Russia, South Korea and Mexico. It is devoted to the detection of ultra high-energy cosmic particles with energies E>7x1019eV, which are revealed through emission in the atmosphere of Cherenkov and fluorescence light in the near-UV region. Current experiments are all ground-based. A big enhancement would rise from space, since a bigger atmospheric target could be monitored. However, since at these high energies the signal is faint and the probability of detection is very low (~1 Km-2 century-1), the optical system must have a large aperture, wide Field of View (FoV) and be necessarily lightweight. This project is the continuation of the EUSO mission, led by ESA, stopped some years ago at the end of phase A, and JEM-EUSO is currently at the end of phase A. For both experiments, a ~2.3 m Entrance Pupil (EP) diameter and a 60° FoV were required to achieve the science goals. However, for the present configuration, the constraint of the maximum stowable dimensions of the JAXA's H-II Transfer Vehicle (HTV) unpressurized cargo area forces the instrument to have maximum transverse dimensions of 2.65 x 1.9 m2. Reflective optics, in the form of a properly designed Schmidt camera, are not yet suitable for this purpose, since these optical requirements would need a large, deployable, primary mirror. The main challenge for designing the current configuration consists in developing an unusual combination of large and lightweight refractive optics: two double-sided curved Fresnel lenses and a central curved Fresnel + diffractive lens, in UV-grade PMMA and/or CYTOP, have been considered. This paper describes the development of such a system, focusing on the possible choices of materials and overall optical design, which is responsibility of the authors. Performances of the latest configurations are also presented.","PeriodicalId":237474,"journal":{"name":"International Conference on Space Optics — ICSO 2010","volume":"63 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-09-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"123317647","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

{"title":"Multilayer coatings for METIS instrument","authors":"A. Corso, P. Zuppella, G. Monaco","doi":"10.1117/12.2552596","DOIUrl":"https://doi.org/10.1117/12.2552596","url":null,"abstract":"The Multi Element Telescope for Imaging and Spectroscopy (METIS) is a coronagraph onboard of Solar Orbiter. It will perform simultaneous observations at HeII Lyman-α line, HI Lyman-α line and in visible. To achieve such capability, instrument mirrors need to be coated by multilayer (ML) structures with high efficiency at all three spectral ranges. Coatings with higher performances with respect standard Mo/Si are desirable. An instrument prototype of METIS has just flown onboard of a NASA sounding rocket: in this case, optics were coated with Mg/SiC MLs. Better performances have been obtained in terms of reflectivity, but long term stability of this coating is an open problem. Moreover the harsh conditions of the environment met during the Solar Orbiter mission given by plasma particles and high temperature could affect the lifetime of the optical components on the long term. We present the design and reflectivity tests of multilayer structures in which performances improvement is obtained by the use of novel capping layers. All multilayers are tuned at 30.4nm line but the design also maximize the performances at 121.6nm and 500 – 650 nm visible range. Analysis of Solar Orbiter environment have been carried on in order to point out the main damaging sources for the nanostructures. Computer simulations with a devoted software have been performed to preliminary evaluation of the possible instabilities in multilayers. Experimental tests for investigating the effects of the thermal heating and particles bombardments in the reflectivity performances have been planned.","PeriodicalId":237474,"journal":{"name":"International Conference on Space Optics — ICSO 2010","volume":"25 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-09-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133263516","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

{"title":"Digital and analogue optoelectronic links for intrasatellite communications","authors":"J. Blasco, O. Navasquillo, C. Sáez","doi":"10.1117/12.2552427","DOIUrl":"https://doi.org/10.1117/12.2552427","url":null,"abstract":"","PeriodicalId":237474,"journal":{"name":"International Conference on Space Optics — ICSO 2010","volume":"38 2 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-09-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"133558999","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

{"title":"400-1000 nm all-dielectric linear variable filters for ultra compact spectrometers","authors":"F. Lemarquis, L. Abel-Tiberini, C. Koç, M. Lequime","doi":"10.1117/12.2552593","DOIUrl":"https://doi.org/10.1117/12.2552593","url":null,"abstract":"","PeriodicalId":237474,"journal":{"name":"International Conference on Space Optics — ICSO 2010","volume":"20 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-09-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"122031581","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

{"title":"LOTIS facility successfully reaches initial operation capability","authors":"R. Bell, Sheldon B. Hutchinson, S. Borota","doi":"10.1117/12.2552428","DOIUrl":"https://doi.org/10.1117/12.2552428","url":null,"abstract":"","PeriodicalId":237474,"journal":{"name":"International Conference on Space Optics — ICSO 2010","volume":"58 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-09-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130484612","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}

{"title":"The STARTIGER'S demonstrators: toward a new generation of formation flying solar coronagraphs","authors":"S. Vives, L. Damé, P. Lamy","doi":"10.1117/12.2552606","DOIUrl":"https://doi.org/10.1117/12.2552606","url":null,"abstract":"","PeriodicalId":237474,"journal":{"name":"International Conference on Space Optics — ICSO 2010","volume":"35 1","pages":"0"},"PeriodicalIF":0.0,"publicationDate":"2019-09-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"130893100","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}