Add to ORKGIssued as Progress report no. 1-28, Final report, and Final report corrected, Project no. E-16-646Final report has title: Probabilistic fracture mechanics and optimum fracture control analytical procedures for a reusable solid rocket motor cas
To increase the success rate of U.S. built Rocket Motors (SRM), the approach taken is: (1) set commo...
Physics-based models are routinely used to predict the performance of engineered systems to make dec...
Current practical approaches used in structural health assessment programs of aerospace structures i...
A methodology for the reliability analysis of a reusable solid rocket motor case is discussed. The a...
Development of a procedure for the reliability analysis of the solid rocket motor case of the space ...
During the structural certification effort for the Space Launch System solid rocket booster nozzle, ...
Designing a reliable system is difficult and costly, due to the design process to be followed and te...
A recent article in Aerospace America claims that 'the average success ratio of the current U.S. sta...
To be competitive in the market, it is very important to design cost effective and reliable products...
Current practical approaches used in structural health assessment programs of aerospace structures i...
This paper provides an overview of an improved probabilistic fracture mechanics (PFM) model used for...
Structural integrity evaluation of military systems is vital in such applications as rocket launcher...
An improved methodology for quantitatively evaluating failure risk of spaceflight systems to assess ...
We develop a case breach model for the on-board fault diagnostics and prognostics system for sub-sca...
The concepts explored in a state of the art review of those engineering fracture mechanics considere...
To increase the success rate of U.S. built Rocket Motors (SRM), the approach taken is: (1) set commo...
Physics-based models are routinely used to predict the performance of engineered systems to make dec...
Current practical approaches used in structural health assessment programs of aerospace structures i...
A methodology for the reliability analysis of a reusable solid rocket motor case is discussed. The a...
Development of a procedure for the reliability analysis of the solid rocket motor case of the space ...
During the structural certification effort for the Space Launch System solid rocket booster nozzle, ...
Designing a reliable system is difficult and costly, due to the design process to be followed and te...
A recent article in Aerospace America claims that 'the average success ratio of the current U.S. sta...
To be competitive in the market, it is very important to design cost effective and reliable products...
Current practical approaches used in structural health assessment programs of aerospace structures i...
This paper provides an overview of an improved probabilistic fracture mechanics (PFM) model used for...
Structural integrity evaluation of military systems is vital in such applications as rocket launcher...
An improved methodology for quantitatively evaluating failure risk of spaceflight systems to assess ...
We develop a case breach model for the on-board fault diagnostics and prognostics system for sub-sca...
The concepts explored in a state of the art review of those engineering fracture mechanics considere...
To increase the success rate of U.S. built Rocket Motors (SRM), the approach taken is: (1) set commo...
Physics-based models are routinely used to predict the performance of engineered systems to make dec...
Current practical approaches used in structural health assessment programs of aerospace structures i...