Share Email Print

Proceedings Paper

Optical design of the composite infrared spectrometer (CIRS) for the Cassini mission
Author(s): Peter William Maymon; Michael G. Dittman; Bert A. Pasquale; Donald E. Jennings; Kimberly I. Mehalick; Catherine J. Trout
Format Member Price Non-Member Price
PDF $17.00 $21.00

Paper Abstract

The Composite Infrared Spectrometer (CIRS) is an instrument currently under development at NASA Goddard Space Flight Center for the Cassini mission to Saturn. The CIRS optical design heritage extends back to the Infrared Interferometer Spectrometer (IRIS) which flew on Voyager. CIRS is the next logical step in the exploration of the atmosphere of Saturn and Titan. It will obtain more complete sets of data with broader spectral coverage, higher spectral and spatial resolution, and greater sensitivity. The CIRS optical design consists of four subassemblies: (1) a 50.8 cm diameter Cassegrain telescope, (2) a Mid-Infrared (MIR) Michelson interferometer, (3) a Far-Infrared (FIR) polarizing interferometer, and (4) a Reference interferometer (RI).

Paper Details

Date Published: 1 November 1993
PDF: 12 pages
Proc. SPIE 1945, Space Astronomical Telescopes and Instruments II, (1 November 1993); doi: 10.1117/12.158752
Show Author Affiliations
Peter William Maymon, NASA Goddard Space Flight Ctr. (United States)
Michael G. Dittman, Swales & Associates, Inc. (United States)
Bert A. Pasquale, Swales & Associates, Inc. (United States)
Donald E. Jennings, NASA Goddard Space Flight Ctr. (United States)
Kimberly I. Mehalick, Advanced Technology & Research Corp. (United States)
Catherine J. Trout, NASA Goddard Space Flight Ctr. (United States)

Published in SPIE Proceedings Vol. 1945:
Space Astronomical Telescopes and Instruments II
Pierre Y. Bely; James B. Breckinridge, Editor(s)

© SPIE. Terms of Use
Back to Top