The results of numerical simulations of a compact steel impactor with the aluminum porous shields under high-speed shock loading are presented. The porosity of barrier varies in wide range provided that its mass stays the same, but the impactor has always equal (identical) mass. Here presented the final assessment of the barrier perforation speed depending on its porosity and initial shock speed. The range of initial impact speed varies from 1 to 10 km/s. Physical phenomena such as: destruction, melting, vaporization of a interacting objects are taken into account. The analysis of a shield porosity estimation disclosed that the protection effectiveness of porous shield reveals at the initial impact speed grater then 1.5 km/s, and it increas...
Progress in shield design against space debris can be achieved only when a combined approach based o...
The results of 18 impact tests performed on Whipple shields were compared to the predicted ballistic...
AbstractPorous-ceramic, thermal protection systems were used heavily on the Orbiter, and they are cu...
The results of numerical simulations of a compact steel impactor with the aluminum porous shields un...
In this work the influence of the characteristics ofthematerial ofthe striker (cumulative jet or pr...
In this paper we consider issues related to numerical modelling of processes of high-speed impact ef...
The study represents the analysis of numerical simulation of the failure of aluminum targets made of...
The paper presents a calculation-experimental study on high-speed interaction of the metal projectil...
The development of lightweight protective structures of increased ballistic resistance is not an eas...
A significant amount of research has been conducted in the last decades on the design of spacecraft ...
Starting with an introduction into the field of hypervelocity impacts, an overview over current rese...
For the manufacture of transparent armor of high class protection, as a rule, reinforced silicate gl...
The given article presents the conducted calculation and experimental study on destruction of heat-r...
This thesis investigates the use of porous materials in a multi-layered armor concept. The prototype...
Granular forms of common materials such as metals and ceramics, sands and soils, porous energetic ma...
Progress in shield design against space debris can be achieved only when a combined approach based o...
The results of 18 impact tests performed on Whipple shields were compared to the predicted ballistic...
AbstractPorous-ceramic, thermal protection systems were used heavily on the Orbiter, and they are cu...
The results of numerical simulations of a compact steel impactor with the aluminum porous shields un...
In this work the influence of the characteristics ofthematerial ofthe striker (cumulative jet or pr...
In this paper we consider issues related to numerical modelling of processes of high-speed impact ef...
The study represents the analysis of numerical simulation of the failure of aluminum targets made of...
The paper presents a calculation-experimental study on high-speed interaction of the metal projectil...
The development of lightweight protective structures of increased ballistic resistance is not an eas...
A significant amount of research has been conducted in the last decades on the design of spacecraft ...
Starting with an introduction into the field of hypervelocity impacts, an overview over current rese...
For the manufacture of transparent armor of high class protection, as a rule, reinforced silicate gl...
The given article presents the conducted calculation and experimental study on destruction of heat-r...
This thesis investigates the use of porous materials in a multi-layered armor concept. The prototype...
Granular forms of common materials such as metals and ceramics, sands and soils, porous energetic ma...
Progress in shield design against space debris can be achieved only when a combined approach based o...
The results of 18 impact tests performed on Whipple shields were compared to the predicted ballistic...
AbstractPorous-ceramic, thermal protection systems were used heavily on the Orbiter, and they are cu...