Optimum structural design based on reliability and proof-load testing
Optimal structural weight in design based on reliability analysis and proof-load tests
Shinozuka, M.↗
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Results for “reliablity”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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The improvement of an electronic power supply for greater reliability in aerospace use
Upgrading of electronic power supply for greater reliability in aerospace use
Quitter, J. P.↗
Optimum structural design based on reliability and proof-load test
Optimum structural design based on reliability proof load tests
Shinozuka, M.↗
Assessment of reliability of metal-oxide- silicon devices
Reliability of metal oxide silicon integrated microcircuits
Bagley, B.↗
Reliable information storage in memories designed from unreliable components.
Reliable information storage in memories designed from unreliable components
Taylor, M. G.↗
Reliable computation in computing systems designed from unreliable components.
Reliable computation in computing systems designed from unreliable components, considering two models for component malfunctions
Taylor, M. G.↗
Reliability assessment of microcircuits and microelectronic systems.
Microcircuit components and microelectronic systems reliability assessment including short term testing, noting digital systems, packaging, production controls, etc
Hall, E. C.↗
Reliability and maintainability analysis of a two-year manned spacecraft mission.
Reliability and maintainability analysis of two year spacecraft mission combining earth orbits and Mars program, using computerized mathematical model
Jennings, H. A.↗
Current status of scanning electron microscopy in semiconductor device reliability physics.
Scanning electron microscopy for reliability studies in semiconductor devices
Anstead, R. J.↗
SIRU - A new inertial system concept for inflight reliability and maintainability.
Strapdown inertial reference unit system for inflight reliability and maintainability, discussing design and components
Crisp, R.↗
The impact of failure data on management of a launch operations reliability program.
Failure data role in management of launch operations reliability program
Cato, R. E., Jr.↗
Optimum structural design based on reliability and proof-load test.
Structural design optimization based on reliability analysis stressing proof-load test and weight savings consideration under cost constraint
Shinozuka, M.↗
Design of a long-life reliable nuclear experiment for space flight.
Solid state detector for electron spatial distribution measurements on OGO-F satellite, discussing design emphasizing reliability
Trainor, J. H.↗
A generalized limit theorem for reliability.
Generalized limit theorem for reliability replacing Drenick exponential theorem
Evans, R. A.↗
Optimization by integer programming of constrained reliability problems with several modes of failure.
Integer programming method for optimizing constrained reliability problems with several system failure modes
Tillman, F. A.↗
System availability management technique for reliability and maintainability analysis
Method for total system availability analysis is based on numerical prediction of the reliability, maintainability, and availability of each function system. It incorporates these functional-system estimates into an overall mathematical model.
Davenport, G. K.↗
Optimum structural design based on reliability analysis
Proof-load test improves statistical confidence in the estimate of reliability, numerical examples indicate a definite advantage of the proof-load approach in terms of savings in structural weight. The cost of establishing the statistical distribution of strength of the structural material is also introduced into the cost formulation
Heer, E.↗
Reliability Analysis Model
RAM program determines probability of success for one or more given objectives in any complex system. Program includes failure mode and effects, criticality and reliability analyses, and some aspects of operations, safety, flight technology, systems design engineering, and configuration analyses.
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