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Integration of a Fire Detector into a SpacecraftA detector sensitive to only the ultraviolet radiation emitted by flames has been selected as the basic element of the NASA Skylab fire detection system. It is sensitive to approximately 10(exp -12)W of radiation and will detect small flames at distances in excess of 3m. The performance of the detector was verified by experiments in an aircraft flying zero-gravity parabolas to simulate the characteristics of a fire which the detector must sense. Extensive investigation and exacting design was necessary to exclude all possible sources of false alarms. Optical measurements were made on all the spacecraft windows to determine the amount of solar radiation transmitted. The lighting systems and the onboard experiments also were appraised for ultraviolet emissions. Proton-accelerator tests were performed to determine the interaction of the Earth's trapped radiation belts with the detectors and the design of the instrument was modified to negate these effects.
Document ID
20150018213
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Linford, R. M. F.
(McDonnell-Douglas Corp. Saint Louis, MO, United States)
Date Acquired
September 23, 2015
Publication Date
September 1, 1972
Publication Information
Publication: Journal of Spacecraft
Volume: 9
Issue: 9
Subject Category
Space Transportation And Safety
Spacecraft Instrumentation And Astrionics
Meeting Information
Meeting: Fall Meeting of the Optical Society of America
Location: Ottawa
Country: Canada
Start Date: October 5, 1971
End Date: October 8, 1971
Sponsors: Optical Society of America
Funding Number(s)
CONTRACT_GRANT: NAS9-6555
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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