Abstract: A method and system of applying a security vulnerability assessment of a software program. The method comprises directing, from a security assessing server, to a software program under execution, a plurality of attack vectors, diagnosing a set of results associated with the software program under execution as comprising a security vulnerability, the set of results produced based at least in part on the plurality of attack vectors, and assessing a monetary premium of a risk insurance policy merited by an enterprise based at least in part on a level of control ceded to an attacker in accordance with the set of results.

Abstract: A method and system of applying a security vulnerability assessment of a software program. The method comprises directing, from a security assessing server, to a software program under execution, a plurality of attack vectors, diagnosing a set of results associated with the software program under execution as comprising a security vulnerability, the set of results produced based at least in part on the plurality of attack vectors, and assessing a monetary premium of a risk insurance policy merited by an enterprise based at least in part on a level of control ceded to an attacker in accordance with the set of results.

Abstract: A method and system for dynamic testing and diagnostic assessment of security vulnerability of cloud-based enterprise software applications. The method comprises directing, to a software program under execution, a series of attack vectors; diagnosing a set of results associated with the software execution as comprising one of a security vulnerability and not a security vulnerability, the set of results produced based at least in part on the attack vectors; and assessing a dynamic security vulnerability score for the software program based at least in part on the diagnosing.

Abstract: Guide systems for installing aircraft structures are disclosed. An example apparatus includes a first guide structured to be supported by a first hinge component of a first aircraft structure and a second guide structured to be supported by a second hinge component of a second aircraft structure. The first guide is to receive the second guide when the second structure is at an installation angle relative to the first structure. Engagement between the first guide and the second guide to enable rotational movement of the first hinge component and the second hinge component when the second aircraft structure moves to an installed position.

Abstract: A method and system for dynamic testing and diagnostic assessment of security vulnerability of cloud-based enterprise software applications. The method comprises directing, to a software program under execution, a series of attack vectors; diagnosing a set of results associated with the software execution as comprising one of a security vulnerability and not a security vulnerability, the set of results produced based at least in part on the attack vectors; and assessing a dynamic security vulnerability score for the software program based at least in part on the diagnosing.

Abstract: A spiral conveyor comprising a support frame mounted on a base, a plurality of arcuate conveyor sections interconnected to form a helical conveyor having at least one entrance and one discharge, each of said conveyor sections having a plurality of self-driven conveyor rollers, each of said rollers being activated to rotate in clockwise or counterclockwise direction at a selectable speed, sensor means positioned on selected conveyor sections for detecting the presence of a load in such section, and control logic means for operating said rollers in either an upward or a downward direction.