Deutsch
 
Hilfe Datenschutzhinweis Impressum
  DetailsucheBrowse

Datensatz

 
 
DownloadE-Mail
  Preliminary calibration results of the wide angle camera of the imaging instrument OSIRIS for the Rosetta mission

Deppo, V. D., Naletto, G., Nicolosi, P., Zambolin, P., Cecco, M. D., Debei, S., et al. (2017). Preliminary calibration results of the wide angle camera of the imaging instrument OSIRIS for the Rosetta mission. In Proceedings Volume 10568, International Conference on Space Optics — ICSO 2004. doi:10.1117/12.2308021.

Item is

Basisdaten

einblenden: ausblenden:
Genre: Konferenzbeitrag

Externe Referenzen

einblenden:

Urheber

einblenden:
ausblenden:
 Urheber:
Deppo, V. Da, Autor
Naletto, G., Autor
Nicolosi, P., Autor
Zambolin, P., Autor
Cecco, M. De, Autor
Debei, S., Autor
Parzianello, G., Autor
Ramous, P., Autor
Zaccariotto, M., Autor
Fornasier, S., Autor
Verani, S., Autor
Thomas, N., Autor
Barthol, Peter1, Autor           
Hviid, Stubbe F.2, Autor           
Sebastian, I., Autor
Meller, Reinhard1, Autor           
Sierks, Holger2, Autor           
Keller, Horst Uwe2, Autor           
Barbieri, C., Autor
Angrilli, F., Autor
Lamy, P., AutorRodrigo, R., AutorRickman, H., AutorWenzel, K. P., Autor mehr..
Affiliations:
1Department Sun and Heliosphere, Max Planck Institute for Solar System Research, Max Planck Society, ou_1832289              
2Department Planets and Comets, Max Planck Institute for Solar System Research, Max Planck Society, ou_1832288              

Inhalt

einblenden:
ausblenden:
Schlagwörter: -
 Zusammenfassung: Rosetta is one of the cornerstone missions of the European Space Agency for having a rendezvous with the comet 67P/Churyumov-Gerasimenko in 2014. The imaging instrument on board the satellite is OSIRIS (Optical, Spectroscopic and Infrared Remote Imaging System), a cooperation among several European institutes, which consists of two cameras: a Narrow (NAC) and a Wide Angle Camera (WAC). The WAC optical design is an innovative one: it adopts an all reflecting, unvignetted and unobstructed two mirror configuration which allows to cover a 12° × 12° field of view with an F/5.6 aperture and gives a nominal contrast ratio of about 10–4. The flight model of this camera has been successfully integrated and tested in our laboratories, and finally has been integrated on the satellite which is now waiting to be launched in February 2004. In this paper we are going to describe the optical characteristics of the camera, and to summarize the results so far obtained with the preliminary calibration data. The analysis of the optical performance of this model shows a good agreement between theoretical performance and experimental results.

Details

einblenden:
ausblenden:
Sprache(n): eng - English
 Datum: 2018-05-072017
 Publikationsstatus: Online veröffentlicht
 Seiten: -
 Ort, Verlag, Ausgabe: -
 Inhaltsverzeichnis: -
 Art der Begutachtung: Expertenbegutachtung
 Identifikatoren: DOI: 10.1117/12.2308021
 Art des Abschluß: -

Veranstaltung

einblenden:
ausblenden:
Titel: 5th International Conference on Space Optics 2004
Veranstaltungsort: Toulouse, France
Start-/Enddatum: 2004-03-30 - 2004-04-02

Entscheidung

einblenden:

Projektinformation

einblenden:

Quelle 1

einblenden:
ausblenden:
Titel: Proceedings Volume 10568, International Conference on Space Optics — ICSO 2004
Genre der Quelle: Konferenzband
 Urheber:
Affiliations:
Ort, Verlag, Ausgabe: -
Seiten: - Band / Heft: - Artikelnummer: 105680N Start- / Endseite: - Identifikator: -