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1
Content available remote Ocena niezawodności szkolenia specjalistów logistyki na przykładzie systemu rakietowego „Homar”
Figurski J., Niepsuj J.
Gospodarka Materiałowa i Logistyka
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2017
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nr 5
150--159
PL
W artykule przedstawiono koncepcję oceny szkolenia specjalistów LOGISTYKI zdolnych do wykonywania zadań w ramach łańcucha logistycznego. Wykonywanie zadań logistycznych powierzane jest zespołowi, który przestrzegając reguł wykonawczych doprowadza do realizacji zadania. Z reguły zespół ten składa się z podzespołów, które odpowiedzialne są za realizację przydzielonych zadań. Wykorzystując strukturę niezawodnościową funkcjonowania podzespołów i nałożone wymagania czasowe, dokonywana jest ocena funkcjonowania podzespołów i całego zespołu logistycznego.
EN
The article presents the concept of evaluation of training of LOGISTICS specialists capable of carrying out tasks within the logistic chain. Performing logistic tasks is entrusted to a team that adheres to the implementing rules to accomplish the task. As a rule, this team consists of sub-assemblies that are responsible for accomplishing the assigned tasks. By using the reliability structure of the components and the time requirements imposed, the performance of the components and the entire logistic unit is evaluated.
2
Content available Logistic support of "Homar" rocket system
Figurski J.
Journal of KONES
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2011
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Vol. 18, No. 1
143-148
EN
In paper was showed structure of "Homar" rocket system, its technical equipment and need of logistic support. In that support it is taken into account need of maintenance of systems on specified level of reliability. Together with logistic support it was stressed need of economic support within life cycle of rocket system. Particular attention is taken to repair processes applicable in peace time and within operation. In the peace time it was taken into account service and repair abilities arising from structure like service and repair planned arising from parameters characteristic for given kind of equipment. Similar procedures of service and repair were showed for operation. During the peace time there are standard procedures and equipment but during operation there is necessity of using special repair workshops. It was proposed workshop of special repair on the wheeled chassis and vehicle of technical support designated for temporary repairs and evacuation of damaged equipment to point of gathering that equipment. There were proposed specialists to conducting service and repair works in mentioned workshops. For transportation of weapon system (rockets) was proposed vehicle with ability of loading and unloading on itself and/or launch. In service and repair and loading/unloading processes were proposed proper systems of security of works. Great attention in work was dedicated to problems of logistic support of fire system (launch). It concern of commanding systems, executive systems and commanding superior and subordinate subsystems. Those commanding modules/vehicles which should be technically efficient are the subject of service and repair processes similarly to basic modules. Separate problem of logistic support are subsystems enable gathering of additional information from reconnaissance UAVs and meteorology support. Logistic support of system was proposed taking into account life cycle of fire system module. In that process it was dedicated great attention to acquisition stage with using of tender as the main way to get lowest costs. In the maintenance stage in particular was stressed service and repair processes. At the end of maintaining stage of fire system there are proposed conditions concerned with disposal and/or recycling. That work emphasizes practical attitude from logistic support point of view in application aspect. It is also proposed that the problem of logistic support should be enclosed to general system of management of maintenance processes which encompass of land forces equipment.
3
Content available remote Wpływ struktury układu prowadnica - rakieta na działanie zestawu przeciwlotniczego. Część 2 - Analiza numeryczna
Dziopa Z.
Zeszyty Naukowe Politechniki Rzeszowskiej. Mechanika
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2005
|
z. 65 [222]
91-98
EN
A self-propelled anti-aircraft rocket system is presented in the paper. The system consists of a target-homing short-range missile launcher, a ground vehicle and a driver. The driver activates the process of launching of the two rockets consecutively. The aim of the paper is to discuss the influence of the launcher guide-missile system structure on the anti-aircraft rocket system.
4
Content available remote Wpływ struktury układu prowadnica - rakieta na działanie zestawu przeciwlotniczego. Część 1 - Modelowanie fizyczne i matematyczne
Dziopa Z.
Zeszyty Naukowe Politechniki Rzeszowskiej. Mechanika
|
2005
|
z. 65 [222]
83-90
EN
A self-propelled anti-aircraft rocket system is presented in the paper. The system consists of a target-homing short-range missile launcher, a ground vehicle and a driver. The driver activates the process of launching of the two rockets consecutively. The aim of the paper is to discuss the influence of the launcher guide-missile system structure on the anti-aircraft rocket system.
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