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JWST FGS & NIRISS CVAC Tests November 1, 2011 − January 25, 2012. Pierre Chayer , André Martel, Alex Fullerton, Ed Nelan , Kevin Volk, Anand Sivaramakrishnan , Sherie Holfeltz , Van Dixon, Paul Goudfrooij , Deepashri Thatte , Harry Ferguson Comdev Canada, CSA, UdeM , HIA.
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JWST FGS & NIRISS CVAC TestsNovember 1, 2011 − January 25, 2012 Pierre Chayer, André Martel, Alex Fullerton, Ed Nelan, Kevin Volk, AnandSivaramakrishnan, SherieHolfeltz, Van Dixon, Paul Goudfrooij, DeepashriThatte, Harry Ferguson Comdev Canada, CSA, UdeM, HIA FGS: Fine Guidance Sensor NIRISS: Near-InfraRedImager & SlitlessSpectrograph 2012 May 17
100 mm 2 m Fine Guidance Sensor (FGS) Optical Layout Role of FGS: Provides centroids to the Attitude Control System. Pick-Off Mirror Focus Mirror Detectors TMA Mirrors 2012 May 17
FGS Optical Assembly 2012 May 17
FGS at the David Florida Laboratory 2012 May 17
FGS entering chamber 2012 May 17
FGS Optical Assembly 2012 May 17
FGS in chamber 2012 May 17
Optical Ground System Equipment (OGSE) 2012 May 17
Optical Ground System Assembly (OGSE) NIRISS NIRISS 2012 May 17
Floor plan for CVAC test 2012 May 17
Temperature Profile 2012 May 17
Chamber background 2012 May 17
Location of OGSE Spots in G1 2012 May 17
Images of OGSE Sources 2012 May 17
Bad Pixel Maps 2012 May 17
IDENTIFICATION • Identification of the Guide Star. • Full-frame: strip readout: 36 (64x2048) strips, 8 overlaps. • ID strip integration time: 0.32 sec. • Strip readout: read-read-reset-read-readCDS1 and CDS2. • Create two lists of bright objects. • Merge the two lists one list. • Identify guide star and ref. stars Triad algorithm. • Success Guide star is identified. • ID timing: 82.12 sec, G1, 5 stars, 8 candidates. 2012 May 17