Environmental test contribution to spacecraft reliability.
Environmental test contribution to spacecraft reliability, discussing optimizing techniques for planning space hardware involving environmental and system interactions
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Environmental test contribution to spacecraft reliability, discussing optimizing techniques for planning space hardware involving environmental and system interactions
Constrained reliability optimization problems solution by integer programming noting parallel redundancy systems, formulation for standby redundant units and cost minimization
Apollo gyro reliability covering guidance, navigation and control systems, stressing failure mode prediction
Reliability of electrical power subsystem designed for manned spacecraft
System reliability allocation method for optimal solution selection in tradeoff analysis, developing dynamic programming computational algorithm
Optimization of thermionic generator systems of high reliability
Saturn launch vehicles airborne measuring and telemetry instrumentation systems design for reliable operation during short periods
Quality and reliability control of spacecraft toroidal transformers noting material selection, termination techniques, performance testing, etc
Reliability maximization computational procedure for multistage parallel systems subject to multiple nonlinear constraints
Reliability and maintainability analysis of two year spacecraft mission combining earth orbits and Mars program, using computerized mathematical model
Proof-load test eliminates structures with strength less than the proof load and improves the reliability value in analysis. It truncates the distribution function of strength at the proof load, thereby alleviating verification of a fitted distribution function at the lower tail portion where data are usually nonexistent.
Technique based upon matrix representation and matrix collapsing calculates the probability of successfully completing manned missions and of returning the spacecrew safely to earth. This technique provides analytic expressions for each subsystem, making it possible to relate changes in subsystem reliability directly to mission success and crew safety.
NASA methodology for improving reliability and quality of hardware and application to electric power industry
Computerized Arrhenius equation component reliability extrapolation techniques
Study of reliability growth implications of subsystem versus full assembly testing
Computer program for component quality control and reliability data analysis
Quality and reliability assurance research reviews at Marshall Space Flight Center
Quality and reliability standard development and screening test results for MOS microelectronic devices