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A Miniature Solid-State Spectrometer for Space Applications: Field TestsA solid state infrared spectrometer has been developed under the Planetary Instrument Definition and Development Program PIDDP to implement a small rugged spectrometer principally for landed applications. The instrument uses the high index of refraction and waveguide properties of a silicon slab to achieve good spectral resolution and high throughput in a small instrument footprint (less than 25 cm). Light enters the silicon slab and is reflected off a grating (Ebert configuration), utilizing the silicon index of refraction to achieve high dispersion. An array of microthermopiles is used to measure the amplitude of the dispersed light. Input optics are typically utilized to focus light on the input aperture and a chopper is used to compensate system drift.
Document ID
20040062516
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Smythe, W. D.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Johnson, E
(Ion Optics, Inc. Waltham, MA, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2004
Publication Information
Publication: Lunar and Planetary Science XXXV: Missions and Instruments: Hopes and Hope Fulfilled
Subject Category
Lunar And Planetary Science And Exploration
Distribution Limits
Public
Copyright
Public Use Permitted.
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