Engineering topics
Publications and source records attributed to Jaffe, P..
Several tests used to determine adequacy of photovoltaic systems, their modules, and materials to survive in real environments. Tests include outdoor testing of systems, real-time and accelerated outdoor testing of modules and materials, and laboratory testing of modules and materials.
The 12 continental remote sites were decommissioned. Testing was consolidated into a five-site network consisting of the four Southern California sites and a new Florida site. 16 kW of new state-of-the-art modules were deployed at the five sites. Testing of the old modules continued at the Goldstone site but as a low-priority item. Array testing of modules is considered. Additional new testing capabilities were added. A battery-powered array data logger is discussed. A final set of failure and degradation data was obtained from the modules.
An overview of outdoor and laboratory testing being applied to terrestrial photovoltaic modules is presented. Descriptions of the test procedures, examples of results, and discussion of the advantages and shortcomings of each approach are included. The test program consists of real-time outdoor testing of systems, modules and materials, and accelerated outdoor testing and laboratory testing of modules. The test results suggest that the various types of tests complement each other and contribute toward the objective of verifying the environmental suitability of the product. A description of representative photovoltaic systems operational in the U.S. in 1981 is presented, along with an identification, description, and physical inspection summary of JPL test module sites and a summary of degradation and failure data for the modules.
After almost four years of endurance testing of photovoltaic modules, no fundamental life-limiting mechanisms were identified that could prevent the twenty-year life goal from being met. The endure data show a continual decline in the failure rate with each new large-scale procurement. Cracked cells and broken interconnects continue to be the principal causes of failure. Although the modules are more adversely affected physically by hot, humid environments than by cool or dry environments there are insufficient data to correlate failure with environment. There is little connection between the outward physical condition of a module and changes in its electrical performance.
Degradation tests indicate that electrical degradation is not a slow monotonically increasing phenomenon as originally thought but occurs abruptly as the result of some traumatic event. This finding has led to a change in the test philosophy. A discussion of this change is presented along with a summary of degradation and failure data from all the sites and results from a variety of special tests. New instrumentation for in-field measurements are described. Field testing activity was expanded by the addition of twelve remote sites located as far away as Alaska and the Canal Zone. Descriptions of the new sites are included.
Transonic sting interference has been studied in a supersonic wind tunnel to obtain free flight and sting support data on identical models. The two principal configurations, representing fuselage bodies, were cigar shaped with tail fins. The others were a sharp 10-deg cone, a sphere, and a blunt entry body. Comparative data indicated that the sting had an appreciable effect on drag for the fuselage-like configurations; drag rise occurred 0.02 Mach number earlier in free flight, and drag level was 15% greater. The spheres and the blunt bodies were insensitive to the presence of stings regardless of their size. The 10-deg cones were in between, experiencing no drag difference with a minimum diameter sting, but a moderate difference with the largest diameter sting tested. All data tend to confirm the notion that for the more slender bodies the sting not only affects flow but the forebody flow as well.
Results from the first bi-planar wind tunnel free-flight test program designed to investigate the difference between planar and nonplanar dynamic stability are presented. The test provides perhaps the best free-flight angular documentation of arbitrary nonplanar motion yet obtained. Two widely different configurations, a blunt 60-deg cone and a sharp 10-deg half-angle cone, were tested. Comparisons between the angular motion from raw data and the analytical fits indicate a phasing difference. An examination of possible causes discounts experimental errors as an explanation and points strongly toward an inadequacy of the theoretical force model.
Spinning blunt entry vehicles dynamic stability tests in terminal regime, discussing dependence on angle of attack
Missile oscillations in plane during pitching moment hysteresis, discussing test coefficients suitability for predicting motion
Atmospheric entry-capsule dynamics, considering angle of attack motion under gravity forces influence and aerodynamic normal force stability relations
Angle of attack effect on motion throughout entry of spinning descending vehicle, noting effects of transverse angular velocity and spin rate
Solution for angular motion analysis on spinning atmospheric entry vehicle
Tricyclic equation of motion extended because of importance increase of nonplanar free flight testing
Free flight dynamic stability measurements indicate that boundary layer transition has no perceptible effect
Supersonic wind tunnel test data, angle of attack envelope computations, and accelerometer package for reconstructing density profile of unknown atmosphere
Energy integral equation for dynamic stability flight analysis
Wind tunnel techniques used to determine pitch damping at large angles of oscillation for proposed mars atmospheric entry vehicles
Pitch damping at large angles of oscillation for proposed mars atmosphere-entry vehicles - wind tunnel test methods