| Issue |
EAS Publications Series
Volume 34, 2009
Astronomy in the Submillimeter and Far Infrared Domains with the Herschel Space Observatory
|
|
|---|---|---|
| Page(s) | 3 - 20 | |
| DOI | https://doi.org/10.1051/eas:0934001 | |
| Published online | 20 December 2008 | |
L. Pagani and M. Gerin (eds)
EAS Publications Series, 34 (2009) 3-20
The Herschel-Heterodyne Instrument for the Far-Infrared (HIFI)
1
SRON, National Institute for Space Research, Groningen, The Netherlands
2
Leiden Observatory, University of Leiden, The Netherlands
3
CESR, CNRS and Université Paul Sabatier, Toulouse, France
4
Physics Department, CalTech, Pasadena, California, USA
5
KOSMA, University of Köln, Germany
6
NASA, Ames Research Centre, Mountain View, California, USA
7
Max-Planck-Institute für Radio Astronomie, Bonn, Germany
8
IEM-CSIC, Madrid, Spain
9
NASA, Jet Propulsion Laboratories, Pasadena, California, USA
10
Obs. de Yebes, Spain
11
IFSI, via del Fosso del Cavaliere, 00133 Roma, Italie
Abstract
This paper describes the Heterodyne Instrument for the Far-Infrared (HIFI) to be launched onboard of ESA's Herschel Space Observatory, by 2008. The instrument is designed to be electronically tunable over a wide and continuous frequency range in the Far Infrared, with velocity resolutions better than 0.1 km s-1 and a high sensitivity. This will allow detailed investigations of a wide variety of astronomical sources, ranging from solar system objects, star formation regions to nuclei of galaxies. The instrument comprises 5 frequency bands covering 480–1150 GHz with SIS mixers and a sixth dual frequency band, for the 1410–1910 GHz range, with Hot Electron Bolometer Mixers (HEB). The Local Oscillator (LO) subsystem consists of a Ka-band synthesizer followed by 14 chains of frequency multipliers, 2 chains for each frequency band. A pair of Auto-Correlators and a pair of Acousto-Optic spectrometers process the two IF signals from the dual-polarization front-ends to provide instantaneous frequency coverage of 4 GHz, with a set of resolutions (140 kHz to 1 MHz), better than <0.1 km s-1. After a successful qualification program, the flight instrument entered the testing phase. We will also report on the first pre-flight test and calibration results together with the expected in-flight performance.
© EAS, EDP Sciences, 2009
