Add to ORKGAn attempt is made to show that redundancies in some aerospace mechanisms do not generally improve the odds for success. Some of these redundancies may even be the very cause for failure of the system. To illustrate this fallacy, two designs based on the Control of Flexible Structures I (COFS I) Mast deployer and retractor assembly (DRA) are presented together with novel designs to circumvent such design inadequacies, while improving system reliability
The functions of the Control of Flexible Structures I (COFS I) deployer and retractor assembly (DRA)...
Objectives. The relevance of this article lies in the fact that the problem of increasing the reliab...
ABSTRACT This research article deals with different aspects of redundancy techniques at various lev...
The parts of electric motors which should be duplicated in order to provide maximum reliability in s...
Non-serviceable systems are often constrained by three requirements that address the need to reliabl...
The constraint of requiring airplanes to have inherent aerodynamic stability can be removed by using...
Spaceflight mechanisms have a reputation for being difficult to develop and operate successfully. Th...
The flight control systems, designed in order to assure the necessary safety level even in failure c...
Reliability and maintainability requirements for reusable space vehicles are more nearly those for a...
The challenge of providing redundancy management (RM) and fault tolerance to meet the Shuttle Progra...
How much redundancy should be built into a subsystem such as a space power subsystem. How does a rel...
Redundancy is one of the primary techniques for the engineering of safety-critical systems. Back-up ...
The need to improve space mechanism reliability is underscored by a long history of flight failures ...
The goal of this paper is to determine the specific features, which must be taken into consideration...
This paper argues that redundancy in engineering, should be understood as a 'design paradigm' that f...
The functions of the Control of Flexible Structures I (COFS I) deployer and retractor assembly (DRA)...
Objectives. The relevance of this article lies in the fact that the problem of increasing the reliab...
ABSTRACT This research article deals with different aspects of redundancy techniques at various lev...
The parts of electric motors which should be duplicated in order to provide maximum reliability in s...
Non-serviceable systems are often constrained by three requirements that address the need to reliabl...
The constraint of requiring airplanes to have inherent aerodynamic stability can be removed by using...
Spaceflight mechanisms have a reputation for being difficult to develop and operate successfully. Th...
The flight control systems, designed in order to assure the necessary safety level even in failure c...
Reliability and maintainability requirements for reusable space vehicles are more nearly those for a...
The challenge of providing redundancy management (RM) and fault tolerance to meet the Shuttle Progra...
How much redundancy should be built into a subsystem such as a space power subsystem. How does a rel...
Redundancy is one of the primary techniques for the engineering of safety-critical systems. Back-up ...
The need to improve space mechanism reliability is underscored by a long history of flight failures ...
The goal of this paper is to determine the specific features, which must be taken into consideration...
This paper argues that redundancy in engineering, should be understood as a 'design paradigm' that f...
The functions of the Control of Flexible Structures I (COFS I) deployer and retractor assembly (DRA)...
Objectives. The relevance of this article lies in the fact that the problem of increasing the reliab...
ABSTRACT This research article deals with different aspects of redundancy techniques at various lev...