DocumentCode
343950
Title
A dual band telescope for microwave instrument on Rosetta Orbiter (MIRO)
Author
Jamnejad, Vahraz
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume
3
fYear
1999
fDate
1999
Firstpage
265
Abstract
In this paper the requirements, specifications, design procedures, and analytical results for a dual frequency space-based telescope are discussed. The telescope is used as part of the microwave instrument on board the Rosetta Orbiter spacecraft, which will be launched early in the next century to rendezvous with and probe the Comet Wirtanen for water content and other material properties. The Offset-fed Cassegrain telescope reaches two receivers at millimeter (190 GHz) and sub-millimeter (560 GHz) via a beam waveguide arrangement. Gaussian beam and Physical Optics methods have been used in the successful design and analysis of the telescope. The telescope provides far field patterns with good efficiency better than 60%, and very low sidelobes better than 30 dB. RF properties of the telescope at varying temperatures, mechanical tolerances, and other operational situations are discussed
Keywords
aerospace instrumentation; physical optics; radiotelescopes; 190 GHz; 560 GHz; 60 percent; Comet Wirtanen; Gaussian beam; MIRO; RF properties; Rosetta Orbiter spacecraft; beam waveguide; dual-band telescope; dual-frequency space-based telescope; far-field pattern; microwave instrument; millimeter-wave receiver; offset-fed Cassegrain telescope; physical optics; submillimeter-wave receiver; Aircraft manufacture; Dual band; Frequency; Instruments; Material properties; Optical design; Optical waveguides; Probes; Telescopes; Water;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 1999. Proceedings. 1999 IEEE
Conference_Location
Snowmass at Aspen, CO
Print_ISBN
0-7803-5425-7
Type
conf
DOI
10.1109/AERO.1999.789785
Filename
789785
Link To Document