Herschel-SPIRE: design, ground test results, and predicted performance
Author(s) -
Matt Griffin,
B. M. Swinyard,
Laurent Vigroux,
A. Abergel,
P. A. R. Ade,
Philippe André,
J.P. Baluteau,
James J. Bock,
A. Franceschini,
W. K. Gear,
Jason Glenn,
Maohai Huang,
Douglas Griffin,
K. J. King,
E. Lellouch,
David Naylor,
S. J. Oliver,
G. Olofsson,
Ismael Pérez-Four,
M. J. Page,
M. Rowan-Robinson,
Paolo Saraceno,
Eric Sawyer,
Gillian Wright,
A. Zavagno,
Asier Abreu,
G. J. Bendo,
A. A. Mac Dowell,
C. D. Dowell,
Marc Ferlet,
T. Fulton,
Peter Hargrave,
G. T. Laurent,
S. J. Leeks,
Tanya Lim,
Nanyao Lu,
Hien T. Nguyen,
Alan Pearce,
E. T. Polehampton,
Davide Rizzo,
Bernhard Schulz,
S. D. Sidher,
David L. Smith,
Locke D. Spencer,
I. Valtchanov,
Adam L. Woodcraft,
Kevin Xu,
Lijun Zhang
Publication year - 2008
Publication title -
proceedings of spie, the international society for optical engineering/proceedings of spie
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.192
H-Index - 176
eISSN - 1996-756X
pISSN - 0277-786X
DOI - 10.1117/12.788312
Subject(s) - spire (mollusc) , computer science , biology , zoology
SPIRE, the Spectral and Photometric Imaging Receiver, is a submillimetre camera and spectrometer for Herschel. It comprises a three-band camera operating at 250, 350 and 500 µm, and an imaging Fourier Transform Spectrometer covering 194-672 µm. The photometer field of view is 4x8 arcmin., viewed simultaneously in the three bands. The FTS has an approximately circular field of view of 2.6 arcmin. diameter and spectral resolution adjustable between 0.04 and 2 cm-1 (λ/∆λ =20-1000 at 250 µm). Following successful testing in a dedicated facility designed to simulate the in-flight operational conditions, SPIRE has been integrated in the Herschel spacecraft and is now undergoing system-level testing prior to launch. The main design features of SPIRE are revi ewed, the key results of instrument testing are outlined, and a summary of the predicted in-flight performance is given.
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