ASD Technical Report, Numéro 62,Partie 919Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963 |
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Expressions et termes fréquents
0.0 at longer 1.0 at wavelengths 1.0 micron transition 500 the feasible 600 COLLECTOR TEMPERATURE 7090 with various absorptance of 1.0 Aeronautical Systems Division AFSC Proj 7340 aval fr OTS average cutoff wavelength blackbody surface Carnot engine coating proved advantageous coatings with properties Collector surfaces considered concentration factor Cutoff wave determined for maximum Efficiency versus Collector emittance of 0.05 engine under various factor and radia Feasible Coating feasible selective coating heat collection efficiency ideal are recommended ideal coating incl illus include a blackbody long wavelengths micron transition region Nonmetallic Materials Lab Overall Efficiency versus proaching the ideal radiator temperature required for collector selective coating proved short wavelengths solar constant solar power SOLAR-POWERED THER solar-powered thermal systems sorber space vehicles Specific research approaches Stefan-Boltzmann constant surfaces considered include surfaces of solar-powered T₂ Temperature with Average vehicles uses FORTRAN versus Collector Temperature WATTS CM wavelengths shorter Wright-Patterson AFB