The infrared space observatory
Abstract The Infrared Space Observatory (ISO), a programme of the European Space Agency, is an astronomical satellite operating at wavelength from 2.5 to 200 μm. It will be launched in 1995. The ISO optical subsystem is a cryogenically cooled telescope with its baffling system (main baffle and sunsh...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Singer, C. [verfasserIn] |
|---|
| Format: |
Artikel |
|---|---|
| Sprache: |
Englisch |
| Erschienen: |
1995 |
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| Schlagwörter: |
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| Anmerkung: |
© Kluwer Academic Publishers 1995 |
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| Übergeordnetes Werk: |
Enthalten in: Space science reviews - Kluwer Academic Publishers, 1962, 74(1995), 1-2 vom: Okt., Seite 67-72 |
|---|---|
| Übergeordnetes Werk: |
volume:74 ; year:1995 ; number:1-2 ; month:10 ; pages:67-72 |
| Links: |
|---|
| DOI / URN: |
10.1007/BF00751253 |
|---|
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OLC2033677702 |
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| 520 | |a Abstract The Infrared Space Observatory (ISO), a programme of the European Space Agency, is an astronomical satellite operating at wavelength from 2.5 to 200 μm. It will be launched in 1995. The ISO optical subsystem is a cryogenically cooled telescope with its baffling system (main baffle and sunshade). The telescope, a 60 cm Ritchey-Chrétien type, focuses the beam to the four scientific instruments located in its focal plane. The extremely low temperature, 1.8 K, is provided by the payload module (PLM) cryostat, filled with superfluid He. This paper presents the main choices done for the telescope design together with their rationale and the performances achieved on the flight model (FM) of the telescope. The FM telescope is presently installed inside the payload module, ready for the system final verifications. | ||
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10.1007/BF00751253 doi (DE-627)OLC2033677702 (DE-He213)BF00751253-p DE-627 ger DE-627 rakwb eng 600 VZ 16,12 ssgn Singer, C. verfasserin aut The infrared space observatory 1995 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Kluwer Academic Publishers 1995 Abstract The Infrared Space Observatory (ISO), a programme of the European Space Agency, is an astronomical satellite operating at wavelength from 2.5 to 200 μm. It will be launched in 1995. The ISO optical subsystem is a cryogenically cooled telescope with its baffling system (main baffle and sunshade). The telescope, a 60 cm Ritchey-Chrétien type, focuses the beam to the four scientific instruments located in its focal plane. The extremely low temperature, 1.8 K, is provided by the payload module (PLM) cryostat, filled with superfluid He. This paper presents the main choices done for the telescope design together with their rationale and the performances achieved on the flight model (FM) of the telescope. The FM telescope is presently installed inside the payload module, ready for the system final verifications. Focal Plane Scientific Instrument European Space Agency Space Observatory Infrared Space Observatory Enthalten in Space science reviews Kluwer Academic Publishers, 1962 74(1995), 1-2 vom: Okt., Seite 67-72 (DE-627)129086606 (DE-600)4860-4 (DE-576)014420724 0038-6308 nnns volume:74 year:1995 number:1-2 month:10 pages:67-72 https://doi.org/10.1007/BF00751253 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-AST SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_24 GBV_ILN_40 GBV_ILN_47 GBV_ILN_70 GBV_ILN_2002 GBV_ILN_2279 GBV_ILN_2286 GBV_ILN_4012 GBV_ILN_4046 GBV_ILN_4082 GBV_ILN_4103 GBV_ILN_4306 GBV_ILN_4700 AR 74 1995 1-2 10 67-72 |
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10.1007/BF00751253 doi (DE-627)OLC2033677702 (DE-He213)BF00751253-p DE-627 ger DE-627 rakwb eng 600 VZ 16,12 ssgn Singer, C. verfasserin aut The infrared space observatory 1995 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Kluwer Academic Publishers 1995 Abstract The Infrared Space Observatory (ISO), a programme of the European Space Agency, is an astronomical satellite operating at wavelength from 2.5 to 200 μm. It will be launched in 1995. The ISO optical subsystem is a cryogenically cooled telescope with its baffling system (main baffle and sunshade). The telescope, a 60 cm Ritchey-Chrétien type, focuses the beam to the four scientific instruments located in its focal plane. The extremely low temperature, 1.8 K, is provided by the payload module (PLM) cryostat, filled with superfluid He. This paper presents the main choices done for the telescope design together with their rationale and the performances achieved on the flight model (FM) of the telescope. The FM telescope is presently installed inside the payload module, ready for the system final verifications. Focal Plane Scientific Instrument European Space Agency Space Observatory Infrared Space Observatory Enthalten in Space science reviews Kluwer Academic Publishers, 1962 74(1995), 1-2 vom: Okt., Seite 67-72 (DE-627)129086606 (DE-600)4860-4 (DE-576)014420724 0038-6308 nnns volume:74 year:1995 number:1-2 month:10 pages:67-72 https://doi.org/10.1007/BF00751253 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-AST SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_24 GBV_ILN_40 GBV_ILN_47 GBV_ILN_70 GBV_ILN_2002 GBV_ILN_2279 GBV_ILN_2286 GBV_ILN_4012 GBV_ILN_4046 GBV_ILN_4082 GBV_ILN_4103 GBV_ILN_4306 GBV_ILN_4700 AR 74 1995 1-2 10 67-72 |
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10.1007/BF00751253 doi (DE-627)OLC2033677702 (DE-He213)BF00751253-p DE-627 ger DE-627 rakwb eng 600 VZ 16,12 ssgn Singer, C. verfasserin aut The infrared space observatory 1995 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Kluwer Academic Publishers 1995 Abstract The Infrared Space Observatory (ISO), a programme of the European Space Agency, is an astronomical satellite operating at wavelength from 2.5 to 200 μm. It will be launched in 1995. The ISO optical subsystem is a cryogenically cooled telescope with its baffling system (main baffle and sunshade). The telescope, a 60 cm Ritchey-Chrétien type, focuses the beam to the four scientific instruments located in its focal plane. The extremely low temperature, 1.8 K, is provided by the payload module (PLM) cryostat, filled with superfluid He. This paper presents the main choices done for the telescope design together with their rationale and the performances achieved on the flight model (FM) of the telescope. The FM telescope is presently installed inside the payload module, ready for the system final verifications. Focal Plane Scientific Instrument European Space Agency Space Observatory Infrared Space Observatory Enthalten in Space science reviews Kluwer Academic Publishers, 1962 74(1995), 1-2 vom: Okt., Seite 67-72 (DE-627)129086606 (DE-600)4860-4 (DE-576)014420724 0038-6308 nnns volume:74 year:1995 number:1-2 month:10 pages:67-72 https://doi.org/10.1007/BF00751253 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-AST SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_24 GBV_ILN_40 GBV_ILN_47 GBV_ILN_70 GBV_ILN_2002 GBV_ILN_2279 GBV_ILN_2286 GBV_ILN_4012 GBV_ILN_4046 GBV_ILN_4082 GBV_ILN_4103 GBV_ILN_4306 GBV_ILN_4700 AR 74 1995 1-2 10 67-72 |
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10.1007/BF00751253 doi (DE-627)OLC2033677702 (DE-He213)BF00751253-p DE-627 ger DE-627 rakwb eng 600 VZ 16,12 ssgn Singer, C. verfasserin aut The infrared space observatory 1995 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Kluwer Academic Publishers 1995 Abstract The Infrared Space Observatory (ISO), a programme of the European Space Agency, is an astronomical satellite operating at wavelength from 2.5 to 200 μm. It will be launched in 1995. The ISO optical subsystem is a cryogenically cooled telescope with its baffling system (main baffle and sunshade). The telescope, a 60 cm Ritchey-Chrétien type, focuses the beam to the four scientific instruments located in its focal plane. The extremely low temperature, 1.8 K, is provided by the payload module (PLM) cryostat, filled with superfluid He. This paper presents the main choices done for the telescope design together with their rationale and the performances achieved on the flight model (FM) of the telescope. The FM telescope is presently installed inside the payload module, ready for the system final verifications. Focal Plane Scientific Instrument European Space Agency Space Observatory Infrared Space Observatory Enthalten in Space science reviews Kluwer Academic Publishers, 1962 74(1995), 1-2 vom: Okt., Seite 67-72 (DE-627)129086606 (DE-600)4860-4 (DE-576)014420724 0038-6308 nnns volume:74 year:1995 number:1-2 month:10 pages:67-72 https://doi.org/10.1007/BF00751253 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-AST SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_24 GBV_ILN_40 GBV_ILN_47 GBV_ILN_70 GBV_ILN_2002 GBV_ILN_2279 GBV_ILN_2286 GBV_ILN_4012 GBV_ILN_4046 GBV_ILN_4082 GBV_ILN_4103 GBV_ILN_4306 GBV_ILN_4700 AR 74 1995 1-2 10 67-72 |
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10.1007/BF00751253 doi (DE-627)OLC2033677702 (DE-He213)BF00751253-p DE-627 ger DE-627 rakwb eng 600 VZ 16,12 ssgn Singer, C. verfasserin aut The infrared space observatory 1995 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Kluwer Academic Publishers 1995 Abstract The Infrared Space Observatory (ISO), a programme of the European Space Agency, is an astronomical satellite operating at wavelength from 2.5 to 200 μm. It will be launched in 1995. The ISO optical subsystem is a cryogenically cooled telescope with its baffling system (main baffle and sunshade). The telescope, a 60 cm Ritchey-Chrétien type, focuses the beam to the four scientific instruments located in its focal plane. The extremely low temperature, 1.8 K, is provided by the payload module (PLM) cryostat, filled with superfluid He. This paper presents the main choices done for the telescope design together with their rationale and the performances achieved on the flight model (FM) of the telescope. The FM telescope is presently installed inside the payload module, ready for the system final verifications. Focal Plane Scientific Instrument European Space Agency Space Observatory Infrared Space Observatory Enthalten in Space science reviews Kluwer Academic Publishers, 1962 74(1995), 1-2 vom: Okt., Seite 67-72 (DE-627)129086606 (DE-600)4860-4 (DE-576)014420724 0038-6308 nnns volume:74 year:1995 number:1-2 month:10 pages:67-72 https://doi.org/10.1007/BF00751253 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-AST SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_24 GBV_ILN_40 GBV_ILN_47 GBV_ILN_70 GBV_ILN_2002 GBV_ILN_2279 GBV_ILN_2286 GBV_ILN_4012 GBV_ILN_4046 GBV_ILN_4082 GBV_ILN_4103 GBV_ILN_4306 GBV_ILN_4700 AR 74 1995 1-2 10 67-72 |
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Abstract The Infrared Space Observatory (ISO), a programme of the European Space Agency, is an astronomical satellite operating at wavelength from 2.5 to 200 μm. It will be launched in 1995. The ISO optical subsystem is a cryogenically cooled telescope with its baffling system (main baffle and sunshade). The telescope, a 60 cm Ritchey-Chrétien type, focuses the beam to the four scientific instruments located in its focal plane. The extremely low temperature, 1.8 K, is provided by the payload module (PLM) cryostat, filled with superfluid He. This paper presents the main choices done for the telescope design together with their rationale and the performances achieved on the flight model (FM) of the telescope. The FM telescope is presently installed inside the payload module, ready for the system final verifications. © Kluwer Academic Publishers 1995 |
| abstractGer |
Abstract The Infrared Space Observatory (ISO), a programme of the European Space Agency, is an astronomical satellite operating at wavelength from 2.5 to 200 μm. It will be launched in 1995. The ISO optical subsystem is a cryogenically cooled telescope with its baffling system (main baffle and sunshade). The telescope, a 60 cm Ritchey-Chrétien type, focuses the beam to the four scientific instruments located in its focal plane. The extremely low temperature, 1.8 K, is provided by the payload module (PLM) cryostat, filled with superfluid He. This paper presents the main choices done for the telescope design together with their rationale and the performances achieved on the flight model (FM) of the telescope. The FM telescope is presently installed inside the payload module, ready for the system final verifications. © Kluwer Academic Publishers 1995 |
| abstract_unstemmed |
Abstract The Infrared Space Observatory (ISO), a programme of the European Space Agency, is an astronomical satellite operating at wavelength from 2.5 to 200 μm. It will be launched in 1995. The ISO optical subsystem is a cryogenically cooled telescope with its baffling system (main baffle and sunshade). The telescope, a 60 cm Ritchey-Chrétien type, focuses the beam to the four scientific instruments located in its focal plane. The extremely low temperature, 1.8 K, is provided by the payload module (PLM) cryostat, filled with superfluid He. This paper presents the main choices done for the telescope design together with their rationale and the performances achieved on the flight model (FM) of the telescope. The FM telescope is presently installed inside the payload module, ready for the system final verifications. © Kluwer Academic Publishers 1995 |
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| title_short |
The infrared space observatory |
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https://doi.org/10.1007/BF00751253 |
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2024-07-03T17:58:29.491Z |
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