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Thermal design and test results for SUNLITE ultra-stable reference cavitySUNLITE (Stanford University-NASA Laser In-Space Technology Experiment) is a space-based experiment which uses a reference cavity to provide a stable frequency reference for a terahertz laser oscillator. Thermal stability of the cavity is a key factor in attaining a stable narrow-linewidth laser beam. The mount which is used to support and align the cavity will provide thermal isolation from the environment. The baseline requirement for thermal stability of the cavity is 0.025 C/min, but the design is directed toward achieving stability well beyond this requirement to improve the science data gained. A prototype of the cavity mount was fabricated and tested to characterize the thermal performance. The thermal vacuum test involved stable high-resolution temperature measurements and stable baseplate temperature control over long durations. Based on test data, the cavity mount design satisfies the severe requirement for the cavity thermal stability.
Document ID
19920002827
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Amundsen, Ruth M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1991
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-104117
NAS 1.15:104117
Report Number: NASA-TM-104117
Report Number: NAS 1.15:104117
Accession Number
92N12045
Funding Number(s)
PROJECT: RTOP 589-01-11-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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