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Parametric analysis report: high temperature solar thermal receiver
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1979 |
| Abstract | A comparison of concept capabilities within the range of interest shows the optimal receiver to be a windowed matrix receiver. The design offers the probability of low production cost, low risk, and compatibility with the most likely identified application, the powering of an advanced (ceramic) Brayton engine to 2600 F. The design permits optional installation of additional thermal buffering mass or a hybrid burner behind the receiver matrix. Thermal buffer (storage) performance would be the best of the several concepts because radiation losses from storage are virtually nonexistent. |
| File Size | 2073686 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19830027253 |
| Archival Resource Key | ark:/13960/t9p27mf3j |
| Language | English |
| Publisher Date | 1979-09-14 |
| Access Restriction | Open |
| Subject Keyword | Approximation Operators (mathematics) Optimization Differential Equations Heredity Nonlinear Equations Optimal Control Spline Functions Convergence Functionals Nonlinear Evolution Equations Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
