NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
High temperature solar photon enginesHigh temperature heat engines designed to make maximum use of the thermodynamic potential of concentrated solar radiation are described. Plasmas between 2000 K and 4000 K can be achieved by volumetric absorption of radiation in alkali metal vapors, leading to thermal efficiencies up to 75% for terrestrial solar power plants and up to 50% for space power plants. Two machines capable of expanding hot plasmas using practical technology are discussed. A binary Rankine cycle uses fluid mechanical energy transfer in a device known as the 'Comprex' or 'energy exchanger.' The second machine utilizes magnetohydrodynamics in a Brayton cycle for space applications. Absorption of solar energy and plasma radiation losses are investigated for a solar superheater using potassium vapor.
Document ID
19780061227
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hertzberg, A.
(Washington Univ. Seattle, WA, United States)
Decher, R.
(Washington Univ. Seattle, WA, United States)
Mattick, A. T.
(Washington, University Seattle, Wash., United States)
Lau, C. V.
(Boeing Commercial Airplane Co. Seattle, Wash., United States)
Date Acquired
August 9, 2013
Publication Date
July 1, 1978
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 78-1177
Meeting Information
Meeting: Fluid and Plasma Dynamics Conference
Location: Seattle, WA
Start Date: July 10, 1978
End Date: July 12, 1978
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
78A45136
Funding Number(s)
CONTRACT_GRANT: NGL-49-002-044
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available