AGENDA 1 - THE INSTRUMENT Architecture of the instrument

Slides:

Advertisements

Similar presentations

ASTEROSEISMOLOGY and SEARCH for EXOPLANETS Vienna - September 18 th 2001 The mission objectives lead to the following requirements at optics level : MAIN.

Advertisements

Leicester SRC, 3-5 Dec 2007 Systems engineering at detector level Tim Stevenson.

Test Cryostat, OGSE and MGSE PACS IHDR: MPE 12/13 Nov 2003 AIV1 PACS Test Cryostat, OGSE and MGSE Gerd Jakob MPE.

1 COROT Science Week, Marseille, 3-6 June 2003 COROT mission Agenda ðSystem progress report §Scenario of observations §Satellite engineering Confirmation.

PPLC/ESA meeting, Feb 27th 2009 Gérad Epstein Patrick Levacher. OVERALL PAYLOAD CONCEPT TRADE-OFFS AT SYSTEM LEVEL PLATO.

SDW20051 Vincent Lapeyrère LESIA – Observatoire de Paris Calibration of flight model CCDs for CoRoT mission.

Cryogenics for B-Pol S. Masi, reporting from F.X. Desert L. Piccirillo …. Use SAMPAN as a baseline, and look for improvements/variations.

PLATO kick-off meeting 09-Nov-2010 PLATO Payload overall architecture.

Page 1HMI Team Meeting – January 26, 2005 HMI Mission Operations Rock Bush HMI Stanford Program Manager Stanford University

PLAnetary Transits and Oscillations of stars Thierry Appourchaux for the PLATO Consortium

SLAC, May 12th, 2004J.L. Puget PLANCK J.L. Puget Institut d'Astrophysique Spatiale Orsay.

SDW2005, juin, Taormina The Corot Space instrument.

PLAnetary Transits and Oscillations of stars PLATO Consortium kick-off meeting.

1 COROT: Scientific comity Sept Calibrations during the commissioning and before the first run. Calibrations cover closed Calibrations cover open.

Eddington Kick-Off. Vienna, September 17th, 2001 T.Muñoz/C.Laviada (INTA) 1 EddiCam: The Eddington Photometric Camera Preliminary Design Layout.

1st Eddington Workshop. Córdoba, June 14th, 2001 J. Miguel Mas-Hesse 1 EddiCam: The Eddington Photometric Camera Preliminary design.

Advanced Concepts & Science Payloads Office Eddicam/EST MeetingPage 1 CCD Procurement Schedule driven Review off-the shelf availability Specific mode of.

The Field Camera Unit Project definition, organization, planning S. Scuderi INAF – Catania.

Presentation EddiCam consortium, FF, Madrid 13/06/2002 Eddington programmatic status Fully approved by SPC as part of ESA’s science program as project.

EddiCam: The Eddington Photometric Camera EddiCam Definition Phase Kick-Off Meeting J. Miguel Mas-Hesse Vienna, 17th Sept., 2001.

SECCHI Consortium Meeting, July 2001 SECCHI Ground Data Systems and Data Processing Nathan Rich NRL/Interferometrics

Corotweek n°9 - ESTEC December 6th, 2005 COROT PROJECT STATUS 1 COROT PROJECT STATUS Thien LAM TRONG.

High Resolution Echelle Spectrograph for Chinese Weihai 1m Telescope. Leiwang, Yongtian Zhu, Zhongwen Hu Nanjing institute of Astronomical Optics Technology.

Solar Probe Plus A NASA Mission to Touch the Sun End to End Test Agenda April 24, 2014 Elena Adams SPP Payload Systems Engineer.

LRR – Mechanical Alphonso Stewart Judy Brannen David Steinfeld Ilene Sokolsky Eric Jenkins.

ASTEROSEISMOLOGY and SEARCH for EXOPLANETS Vienna - September 18 th 2001 Optical performance characterization Point Spread Function (PSF) : Telescope +

1 Leonardo Pinheiro da Silva Corot-Brazil Workshop – October 31, 2004 Corot Instrument Characterization based on in-flight collected data Leonardo Pinheiro.

LIGO-G D LIGO II1 AUX OPTICS SUPPORT Michael Smith, 6/11/03 STRAY LIGHT CONTROL ACTIVE OPTICS COMPENSATION OUTPUT MODE CLEANER PO MIRROR AND PO.

1Corot Science Week, Berlin, December 2003 Inside the COROT machine Overview of global loop for COROT operations Description of COROT Subsystems.

GE+ PL INTERFACES, RESSOURCES PLATO PPLC/ESA meeting, Feb 27th 2009.

Preparing the telescope and CCD-camera for observations Andrych K, Tvardovskyi D.

Optimisation of the PACS Chopper Markus Nielbock Ulrich Klaas Jeroen Bouwman Helmut Dannerbauer Jürgen Schreiber Ulrich Grözinger.

PFP Instrument Status All PFP Instruments Except SWEA have been delivered, integrated, and tested; supporting environmental tests Issues: –EUV alignment.

Kelley Case Concept Design Methods Chief JPL Innovation Foundry Caltech Space Challenge March 24, 2013.

PPLC – ESA FEB 27th 2009 CCD thermal specs G Epstein CCD thermal specifications Divers for Telescope thermal architecture.

Mechanical design meeting, IAG, Calibration Unit mechanical design Svend M. Bauer Andreas Kelz, Emil Popow, Martin M. Roth.

1 System Architecture Mark Herring (Stephen Merkowitz Presenting)

1 Transiting Exoplanet Survey Satellite Daryl Swade Archive Team Meeting June 16, 2014.

1DSM/DAPNIA/SAp – J. MartignacPACS - IHDR - MPE – Nov. 12 – 13, 2003 PACS – IHDR PhFPU Design J. Martignac CEA/DSM/DAPNIA Service d’Astrophysique.

Corot:Ubatuba Nov The Ground Segment: Data Processing. Software development in laboratories. Brazilian contribution. Michel Auvergne Réza Samadi.

V3 SLAC DOE Program Review Gunther Haller SLAC June 13, 07 (650) SNAP Electronics.

NASA Ames Instrumentation Workshop May 13, 2010 Technology / Application Images go here Title of Presentation goes here Description goes here Format. Please.

PACS IBDR MPE 27/28 Feb 2002 AIV 1 PACS IBDR Test Cryostat and OGSE Gerd Jakob MPE.

Wes Ousley June 28, 2001 SuperNova/ Acceleration Probe (SNAP) Thermal.

Spectrograph focal plane 2003 Goals : CCD l Improved CCD Cryostat connections, decoupling, preamp box photodiodes for efficiency monitoring thermistances.

WFIRST Large-cell structure concept design Preview Work in progress 3/4/2016Robin Lafever1.

The Field Camera Unit Results from technical meeting S. Scuderi INAF – Catania.

EUCLID NEAR IR SPECTROGRAPH FOCAL PLANE

SPACE TELESCOPE SCIENCE INSTITUTE Operated for NASA by AURA TIPS / COS 27 June 2002.

Find Cheap Samsung S7 Wallet Case

Status of the SWAP instrument

Rose Navarro HMI Lead Thermal Engineer

Wide-Field Imager for Solar PRobe Plus (WISPR)

The two-point calibration procedure

4x8 Mosaic Camera Development

Development, manufacturing and commercialisation of precision equipment for science

30-Nov-2006 Jean-Marc Defise - CSL

Point Source Transmission Simulations on the COROT baffle

SXC integration and test

COROT, COnvection, ROtation & Transits exoplanétaires

San Diego Conference 2 August 2001

SIDECAR ASIC Characterization Dan Pontillo

Fabio de Oliveira Fialho Michel Auvergne

SLAC DOE Program Review

Launch and On-orbit Checkout

GIFTS Blackbody Subsystem Critical Design Review Blackbody Requirements Flowdown Fred Best 9 March 2004.

Nov. 19, 2009 prepared by H. Matsuhara, N. Takahashi, T. Nakagawa

MAIN CONTRIBUTOR NOISES

- '1:- bs? a ' I.

CHEOPS - CHaracterizing ExOPlanet Satellite

Presentation transcript:

AGENDA 1 - THE INSTRUMENT Architecture of the instrument Functionnal Chains Organization 2 - PHOTOMETRIC PERFORMANCES Mission performance synthesis The noise sources The main contributors Straylight Thermal stability effects on the optico-mecanial structure effects on the CCD and readout electronics Performance needs Thermal concept 3 - GROUND BASED CALIBRATIONS AND INTEGRATIONS Achievable characterizations of the instrument Models CCD test bench

INSTRUMENT MECHANICAL ARCHITECTURE COROT INSTRUMENT IS COMPOSED OF FOUR PRODUCTS COROTEL COROTCAM COROTCASE COROTLOG

TELESCOPE COROTEL product is composed of: AFOCAL External Baffle and protective cover

CAMERA 1) Focal Box 2) Dioptric Objective 3) Shield and adjustment accessories 4) Proximity Electronics boxes (EP) 5) Wiring 6) Thermal control

Electronics units BCC1 BS1. 1 BEX1 BCC2 BS2 BS1. 2 BEX2 MDPU1 BCVCAM BCVETN BCVCAM BS2 BEX2 BEX1