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Shuttle/TDRSS communications system performance analysis
The results of the performance analysis performed on the Shuttle/Tracking and Data Relay Satellite System (TDRSS) communications system are presented. The existing Shuttle/TDRSS link simulation program were modified and refined to model the post-radio frequency interference TDRS hardware and to evaluate the performance degradation due to RFI effects. The refined link models were then used to determine, evaluate and assess expected S-band and Ku-band link performance. Parameterization results are presented for the ground station carrier and timing recovery circuits
Apollo mission D performance analysis of rendezvous charts
Performance analysis of rendezvous charts for Apollo 9 mission
NASA Deep Space Network performance analysis
As part of the Control Center Operations, the Performance Analysis Group has responsibility for validating all committed Deep Space Network support to the various user projects. The group provides the Network with the analysis support necessary to assure that actual Network performance meets or exceeds committed levels throughout the mission. Validation is carried out as the signals are received in real time by monitoring the data streams and comparing the data quality against predicted values and established performance standards and tolerance limits. An important function is to generate the predictions used to point the antennas, acquire the radio frequency, and validate the monitored Network performance. Another function is anomaly investigation. An integral part of validation is the support task of generating and maintaining performance standards and tolerance limits for each flight project. The Performance Analysis Group is broadly divided into two subgroups: real-time personnel and nonreal-time personnel.
Guidance, flight mechanics and trajectory optimization. Volume 17 - Guidance system performance analysis
Methodology used in guidance system performance analysis /assessment/
Past Performance analysis of HPOTP bearings
The past performance analysis conducted on three High Pressure Oxygen Turbopump (HPOTP) bearings from the Space Shuttle Main Engine is presented. Metallurgical analysis of failed bearing balls and races, and wear track and crack configuration analyses were carried out. In addition, one bearing was tested in laboratory at very high axial loads. The results showed that the cracks were surface initiated and propagated into subsurface locations at relatively small angles. Subsurface cracks were much more extensive than was appeared on the surface. The location of major cracks in the races corresponded to high radial loads rather than high axial loads. There was evidence to suggest that the inner races were heated to elevated temperatures. A failure scenario was developed based on the above findings. According to this scenario the HPOTP bearings are heated by a combination of high loads and high coefficient of friction (poor lubrication). Different methods of extending the HPOTP bearing life are also discussed. These include reduction of axial loads, improvements in bearing design, lubrication and cooling, and use of improved bearing materials.
ECAR-6583 Rev 1 Outer Shield Stress and Performance Analysis
Calculations were performed to verify that the Outer Shield Assembly will support the weight of the Water Extended Polyester (WEP) shielding and the lead shielding.
Network performance analysis for the Gemini GTA-8 mission
Network performance analysis for Gemini GTA-8 MISSION
Scout motor performance analysis and prediction study /PAPS/
Scout motor performance analysis and prediction
Apollo mission F performance analysis of rendezvous charts
Computerized simulation and performance analysis of rendezvous charts for Apollo lunar module mission
Computer performance analysis - Applications of accounting data
Computer system performance analysis using accounting data, with availability of data and methods of conditioning and reducing data
A relative performance analysis of atmospheric laser Doppler velocimeter methods.
A performance analysis is presented that compares two remote-sensing atmospheric laser Doppler velocimeter systems, one using dual-scatter and the other local-oscillator illuminating techniques. The comparison results show that there exist specific parameter ranges and conditions whereunder the performance of one of the systems is superior to that of the other. A procedure providing a quantitative basis for a judicious system selection is proposed.
Preliminary thermal performance analysis of the solar Brayton heat receiver
Thermal performance analysis of solar Brayton heat receiver in transferring heat to working gas of Brayton engine
Structural performance analysis and redesign
Program performs stress buckling and vibrational analysis of large, linear, finite-element systems in excess of 50,000 degrees of freedom. Cost, execution time, and storage requirements are kept reasonable through use of sparse matrix solution techniques, and other computational and data management procedures designed for problems of very large size.
Computer performance analysis - Measurement objectives and tools
Objectives and measurements in computer performance analysis
Telecommunications performance analysis and monitoring software
The computer software used for telecommunications performance analysis and monitoring is discussed. The utilization of the TPAP analysis program for the Viking 1975 project and the Voyager 1977 project is described. The functional and design requirements for the successor system, TPAS, are also given.
Performance analysis and data reduction for exascale scientific workflows
Chimbuko is the first in situ, scalable, workflow-level performance analysis tool for trace-level analysis and visualization of application performance. This tool was developed by the Co-design Center for Online Data Analysis and Reduction and funded by the U.S. Department of Energy’s Exascale Computing Project. We provide a detailed description of Chimbuko’s architecture and illustrate our online and offline visualization with multiple use cases. We also present results for the deployment and scalability of the tool as applied to a high-energy physics workflow running at large scale on the Frontier supercomputer.
Performance analysis of the ascent propulsion system of the Apollo spacecraft
Activities involved in the performance analysis of the Apollo lunar module ascent propulsion system are discussed. A description of the ascent propulsion system, including hardware, instrumentation, and system characteristics, is included. The methods used to predict the inflight performance and to establish performance uncertainties of the ascent propulsion system are discussed. The techniques of processing the telemetered flight data and performing postflight performance reconstruction to determine actual inflight performance are discussed. Problems that have been encountered and results from the analysis of the ascent propulsion system performance during the Apollo 9, 10, and 11 missions are presented.