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Study, optimization, and design of a laser heat engineLaser heat engine concepts, proposed for satellite applications, were analyzed to determine which engine concepts best meet the requirements of high efficiency (50 percent or better) continuous operation in space. The best laser heat engine for a near-term experimental demonstration, selected on the basis of high overall operating efficiency, high power-to-weight characteristics, and availability of the required technology, is an Otto/Diesel cycle piston engine using a diamond window to admit CO2 laser radiation. The technology with the greatest promise of scaling to megawatt power levels in the long term is the energy exchanger/gas turbine combination.
Document ID
19780011538
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
January 12, 1978
Subject Category
Lasers And Masers
Report/Patent Number
MSNW-78-1082-1
NASA-CR-152104
Report Number: MSNW-78-1082-1
Report Number: NASA-CR-152104
Accession Number
78N19481
Funding Number(s)
CONTRACT_GRANT: NAS2-9668
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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