Íàöèîíàëüíûé àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé èíñòèòóò”

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß. – 2015. – ¹ 4 (121). – 113 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2015. – ¹ 4 (121). – 113 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2015. – ¹ 4 (121). – 113 ñ.

 

ÑÒÀÒÜè (articleS)

 

Àâòîðû (ÿçûê îðèãèíàëà)

Íàçâàíèå ñòàòüè (article title)

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(pages)

English

Óêðà¿íñüêà ìîâà

Ðóññêèé ÿçûê

Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Äîöåíêî Â. Í.,
Êîâåçà Þ. Â.,
Ëèõîøåðñò È.
 Ã.

SIMPLIFIED dynamic model of high-lift control system

ÑÏÐÎÙÅÍÀ ÌÎÄÅËÜ ÑÈÑÒÅÌÈ ÊÅÐÓÂÀÍÍß ÇÀÊÐÈËÊÀÌÈ ² ÏÅÐÅÄÊÐÈËÊÀÌÈ

ÓÏÐÎÙÅÍÍÀß ÌÎÄÅËÜ ÑÈÑÒÅÌÛ ÓÏÐÀÂËÅÍÈß ÇÀÊÐÛËÊÀÌÈ È ÏÐÅÄÊÐÛËÊÀÌÈ

5–9
(5)

Äàâûäîâà À. Â.

EXPERIMENTAL INVESTIGATIONS OF THE HYDRAULIC RESISTANCE COEFFICIENT OF THE MESH PHASES DELIMITERS IN UNSTEADY LIQUID FLOW

ÅÊÑÏÅÐÈÌÅÍÒÀËÜͲ ÄÎÑË²ÄÆÅÍÍß ÊÎÅÔ²Ö²ªÍÒÓ Ã²ÄÐÀÂ˲×ÍÎÃÎ ÎÏÎÐÓ Ñ²Ò×ÀÑÒÈÕ ÐÎÇIJËÞÂÀײ ÔÀÇ Â ÍÅÑÒÀÖ²ÎÍÀÐÍÎÌÓ Ð²ÄÈÍÍÎÌÓ ÏÎÒÎÖ²

ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÛÅ ÈÑÑËÅÄÎÂÀÍÈß ÊÎÝÔÔÈÖÈÅÍÒÀ ÃÈÄÐÀÂËÈ×ÅÑÊÎÃÎ ÑÎÏÐÎÒÈÂËÅÍÈß ÑÅÒ×ÀÒÛÕ ÐÀÇÄÅËÈÒÅËÅÉ ÔÀÇ Â ÍÅÑÒÀÖÈÎÍÀÐÍÎÌ ÆÈÄÊÎÑÒÍÎÌ ÏÎÒÎÊÅ

1015
(6)

Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ

Øèïóëü Î. Â.

MODERN METHODS OF EDGE FINISHING OF PRECISION PARTS

Ñó÷àñí³ ÌÅÒÎÄÈ Ô²Í²ØÍÎÃÎ ÓÏÎÐßÄÆÅÍÍß ÊÐÀÉÎÊ ÏÐÅÖÈDzÉÍÈÕ ÄÅÒÀËÅÉ

ÑÎÂÐÅÌÅÍÍÛÅ ÌÅÒÎÄÛ ÔÈÍÈØÍÎÉ ÎÒÄÅËÊÈ ÊÐÎÌÎÊ ÏÐÅÖÈÇÈÎÍÍÛÕ ÄÅÒÀËÅÉ

1625
(10)

Äóíàåâ Ä. Â.,
Êðèâîáîêîâ Ë. Â.

Validation of the test types in the process of creating comprehensive development test program for standard integrated launch vehicle

Îáãóíòóâàííÿ âèä³â âèïðîáóâàíü ïðè ñòâîðåíí³ êîìïëåêñíî¿ ïðîãðàìè åêñïåðèìåíòàëüíîãî â³äïðàöþâàííÿ òèïîâî¿ ðàêåòè êîñì³÷íîãî ïðèçà÷åííÿ

ÎÁÎÑÍÎÂÀÍÈÅ ÂÈÄΠÈÑÏÛÒÀÍÈÉ ÏÐÈ ÑÎÇÄÀÍÈÈ ÊÎÌÏËÅÊÑÍÎÉ ÏÐÎÃÐÀÌÌÛ ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÉ ÎÒÐÀÁÎÒÊÈ ÒÈÏÎÂÎÉ ÐÀÊÅÒÛ ÊÎÑÌÈ×ÅÑÊÎÃÎ ÍÀÇÍÀ×ÅÍÈß

2631
(6)

Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ

Ñóááîòà À. Ì.,
Ñèìîíîâ Â. Ô.,
Áû÷êîâà È. Â.

THE EXECUTIVE ORGANS OF SMALL SPACESHIP CONTROL SYSTEMS WITHIN THE FRAMEWORK OF THE “ORBITAL GROUPING” CONCEPTION

ÂÈÁ²Ð ÂÈÊÎÍÀÂ×ÈÕ ÎÐÃÀͲ ÑÈÑÒÅÌ ÓÏÐÀÂ˲ÍÍß ÌÀËÈÕ ÊÎÑ̲×ÍÈÕ ÀÏÀÐÀҲ  ÌÅÆÀÕ ÊÎÍÖÅÏÖ²¯ «ÎÐÁ²ÒÀËÜÍÅ ÓÃÐÓÏÓÂÀÍÍß»

ÈÑÏÎËÍÈÒÅËÜÍÛÅ ÎÐÃÀÍÛ ÑÈÑÒÅÌ ÓÏÐÀÂËÅÍÈß ÌÀËÛÕ ÊÎÑÌÈ×ÅÑÊÈÕ ÀÏÏÀÐÀÒΠ ÐÀÌÊÀÕ ÊÎÍÖÅÏÖÈÈ «ÎÐÁÈÒÀËÜÍÀß ÃÐÓÏÏÈÐÎÂÊÀ»

3237
(6)

Ãåðãåëü È. À.,
Êîðòóíîâ Â. È.

ANALYSIS OF THE FLIGHT OF SMALL UNMANNED AIRCRAFTS FOR PERFORMANCE AERIAL PHOTOGRAPHY OF AREA OBJECTS

ÀÍÀË²Ç ÏÎËÜÎÒÓ ÌÀËÈÕ ÁåÇï³ëîòíèõ ë³òàëüíèõ àïàðàò³â| ÄËß âèêîíàííÿ àåðîôîòîçéîìêè ïëîùàäíèõ îá'ºêò³â

ÀÍÀËÈÇ ÏÎËÅÒÀ ÌÀËÛÕ ÁÅÑÏÈËÎÒÍÛÕ ËÅÒÀÒÅËÜÍÛÕ ÀÏÏÀÐÀÒÎÂ ÄËß ÂÛÏÎËÍÅÍÈß ÀÝÐÎÔÎÒÎÑÚÅÌÊÈ ÏËÎÙÀÄÍÛÕ ÎÁÚÅÊÒÎÂ

3842
(5)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Íàçèí Â. È.

DYNAMIC DESCRIPTIONS OF HYDROSTATODYNAMIC BEARING OF THE DOUBLED TYPE AT DIFFERENT VALUES OF HIS DIAMETER

ÄÈÍÀ̲×Ͳ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ Ã²ÄÐÎÑÒÀÒÎÄÈÍÀ̲×ÍÎÃÎ Ï²ÄØÈÏÍÈÊÀ ÇÄÂΪÍÎÃÎ ÒÈÏÓ ÏÐÈ Ð²ÇÍÈÕ ÇÍÀ×ÅÍÍßÕ ÉÎÃΠIJÀÌÅÒÐÓ

ÄÈÍÀÌÈ×ÅÑÊÈÅ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÃÈÄÐÎÑÒÀÒÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÏÎÄØÈÏÍÈÊÀ ÑÄÂÎÅÍÍÎÃÎ ÒÈÏÀ ÏÐÈ ÐÀÇËÈ×ÍÛÕ ÇÍÀ×ÅÍÈßÕ ÅÃÎ ÄÈÀÌÅÒÐÀ

4346
(4)

Ñâèðèäîâ Â. È.,
Àíäðååâ À. À.

VIBRATION DIAGNOSTICS ROLLING AND SLIDING BEARINGS

²ÁÐÎIJÀÃÍÎÑÒÓÂÀÍÍß Ï²ÄØÈÏÍÈʲ ÊÎ×ÅÍÍß ÒÀ ÊÎÂÇÀÍÍß

ÂÈÁÐÎÄÈÀÃÍÎÑÒÈÐÎÂÀÍÈÅ ÏÎÄØÈÏÍÈÊΠÊÀ×ÅÍÈß È ÑÊÎËÜÆÅÍÈß

4753
(7)

Õàëàòîâ À. À.,
Ñåâåðèí Ñ. Ä.,
Äîíèê Ò. Â.

INFLUENCE PRESSURE LOSS IN THE REGENERATOR HEAT ON EFFICIENCY THERMODYNAMIC CYCLE MODULAR NUCLEAR POWER PLANT WITH HELIUM REACTOR

ÂÏËÈ ÂÒÐÀÒ ÒÈÑÊÓ Â ÐÅÃÅÍÅÐÀÒÎв ÒÅÏËÎÒÈ ÍÀ ÅÔÅÊÒÈÂͲÑÒÜ ÒÅÐÌÎÄÈÍÀ̲×ÍÎÃÎ ÖÈÊËÓ ÌÎÄÓËÜÍί ßÄÅÐÍί ÅÍÅÐÃÅÒÈ×Íί ÓÑÒÀÍÎÂÊÈ Ç ÃÅ˲ªÂÈÌ ÐÅÀÊÒÎÐÎÌ

ÂËÈßÍÈÅ ÏÎÒÅÐÜ ÄÀÂËÅÍÈß Â ÐÅÃÅÍÅÐÀÒÎÐÅ ÒÅÏËÎÒÛ ÍÀ ÝÔÔÅÊÒÈÂÍÎÑÒÜ ÒÅÐÌÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÖÈÊËÀ ÌÎÄÓËÜÍÎÉ ßÄÅÐÍÎÉ ÝÍÅÐÃÅÒÈ×ÅÑÊÎÉ ÓÑÒÀÍÎÂÊÈ Ñ ÃÅËÈÅÂÛÌ ÐÅÀÊÒÎÐÎÌ

5459
(6)

Ñïåñèâöåâ Â. Â.

DIAGNOSTICS OF POWER AND HEAT IMPACT OF SUPERSONIC JET ON BARRIER

IJÀÃÍÎÑÒÈÊÀ ÑÈËÎÂί ÒÀ ÒÅÏËÎÂί IJ¯ ÍÀÄÇÂÓÊÎÂÎÃÎ ÑÒÐÓ̲Íß ÍÀ ÏÅÐÅÏÎÍÓ

ÄÈÀÃÍÎÑÒÈÊÀ ÑÈËÎÂÎÃÎ È ÒÅÏËÎÂÎÃÎ ÂÎÇÄÅÉÑÒÂÈß ÑÂÅÐÕÇÂÓÊÎÂÎÉ ÑÒÐÓÈ ÍÀ ÏÐÅÃÐÀÄÓ

6064
(5)

Ìèòèêîâ Þ. À.,
Êóäåðñêèé Â. Í.,

Êóäà Ñ. À.,
Èâàíèöêèé Ã. Ì.

PROPULSION SYSTEM TANK PRESSURIZATION WITH SOLID FUEL GAS PRODUCER EXPERIMENTAL STUDY

ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÅ ÄÎÑË²ÄÆÅÍÍß ÍÀÄÄÓÂÓ ÁÀʲ ÐÓØ²ÉÍÈÕ ÓÑÒÀÍÎÂÎÊ ÒÂÅÐÄÎÏÀËÈÂÍÈÌÈ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀÌ

ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÅ ÈÑÑËÅÄÎÂÀÍÈÅ ÍÀÄÄÓÂÀ ÁÀÊÎÂ ÄÂÈÃÀÒÅËÜÍÛÕ ÓÑÒÀÍÎÂÎÊ ÒÂÅÐÄÎÒÎÏËÈÂÍÛÌÈ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀÌÈ

6570
(6)

Ðàä÷åíêî Í. È.,
Áîõäàëü Ë.,
Ãðè÷ À. Â.,
Åñèí È. Ï.

INCREASING THE EFFICIENCY OF CLOSED COOLING SYSTEM OF RECIPROCATING GAS ENGINE

ϲÄÂÈÙÅÍÍß ÅÔÅÊÒÈÂÍÎÑÒ² ÑÈÑÒÅÌÈ ÎÁÎÐÎÒÍÎÃÎ ÎÕÎËÎÄÆÅÍÍß ÃÀÇÎÏÎÐØÍÅÂÎÃÎ ÄÂÈÃÓÍÀ

ÏÎÂÛØÅÍÈÅ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÑÈÑÒÅÌÛ ÎÁÎÐÎÒÍÎÃÎ ÎÕËÀÆÄÅÍÈß ÃÀÇÎÏÎÐØÍÅÂÎÃÎ ÄÂÈÃÀÒÅËß

7175
(5)

Ðàä÷åíêî À. Í.,
Êàíòîð Ñ. À.

METODOLOGICAL APROACHES OF RATINAL DESIGNING OF COMBINED WASTE HEAT RECOVERY SYSTEM FOR GAS TURBINE UNIT INTAKE AIR COOLING

ÌÅÒÎÄÎËÎò×ÍÈÉ Ï²ÄÕ²Ä ÄÎ ÐÀÖ²ÎÍÀËÜÍÎÃÎ ÏÐÎÅÊÒÓÂÀÍÍß ÊÎÌÁ²ÍÎÂÀÍί ÒÅÏËÎÂÈÊÎÐÈÑÒÎÂÓÞ×ί ÑÈÑÒÅÌÈ ÎÕÎËÎÄÆÅÍÍß ÏβÒÐß ÍÀ ÂÕÎIJ ÃÀÇÎÒÓÐÁ²ÍÍί ÓÑÒÀÍÎÂÊÈ

ÌÅÒÎÄÎËÎÃÈ×ÅÑÊÈÉ ÏÎÄÕÎÄ Ê ÐÀÖÈÎÍÀËÜÍÎÌÓ ÏÐÎÅÊÒÈÐÎÂÀÍÈÞ ÊÎÌÁÈÍÈÐÎÂÀÍÍÎÉ ÒÅÏËÎÈÑÏÎËÜÇÓÞÙÅÉ ÑÈÑÒÅÌÛ ÎÕËÀÆÄÅÍÈß ÂÎÇÄÓÕÀ ÍÀ ÂÕÎÄÅ ÃÀÇÎÒÓÐÁÈÍÍÎÉ ÓÑÒÀÍÎÂÊÈ

76–79
(4)

Ðàä÷åíêî Ð. Í.,
Êàëèíè÷åíêî È. Â.,
Ùåðáàê Þ. Ã.

TRANSFORMING THE WASTE HEAT OF MARINE DIESEL ENGINE WITH INTAKE AIR COOLING IN CLIMATICAL CONDITIONS OF ROUT LINE

ÒÐÀÍÑÔÎÐÌÀÖ²ß ÑÊÈÄÍί ÒÅÏËÎÒÈ ÑÓÄÍÎÂÎÃÎ ÄÈÇÅËß Ç ÎÕÎËÎÄÆÅÍÍßÌ ÏβÒÐß ÍÀ ÂÕÎIJ  Ê˲ÌÀÒÈ×ÍÈÕ ÓÌÎÂÀÕ ÐÅÉÑÎÂί ˲Ͳ¯

ÒÐÀÍÑÔÎÐÌÀÖÈß ÑÁÐÎÑÍÎÉ ÒÅÏËÎÒÛ ÑÓÄÎÂÎÃÎ ÄÈÇÅËß Ñ ÎÕËÀÆÄÅÍÈÅÌ ÂÎÇÄÓÕÀ ÍÀ ÂÕÎÄÅ Â ÊËÈÌÀÒÈ×ÅÑÊÈÕ ÓÑËÎÂÈßÕ ÐÅÉÑÎÂÎÉ ËÈÍÈÈ

8084
(5)

Ðàä÷åíêî À. Í.,
Ñòàõåëü À.,
Ïðÿäêî À. È.,
Äîëãàíîâ Þ. À.

ACUMULATION AND USING THE CONDENSATE IN THE PROCESSES OF COOLING THE CYCLIC AIR OF GAS ENGINE FOR TRIGENERATION SYSTEM OF INTEGRATED ENERGY SUPPLY

ÀÊÓÌÓËßÖ²ß ÒÀ ÂÈÊÎÐÈÑÒÀÍÍß ÊÎÍÄÅÍÑÀÒÓ Â ÏÐÎÖÅѲ ÎÕÎËÎÄÆÅÍÍß ÖÈÊËÎÂÎÃÎ ÏβÒÐß ÃÀÇÎÂÎÃÎ ÄÂÈÃÓÍÀ ÒÐÈÃÅÍÅÐÀÖ²ÉÍί ÓÑÒÀÍÎÂÊÈ ÀÂÒÎÍÎÌÍÎÃÎ ÅÍÅÐÃÎÇÀÁÅÇÏÅ×ÅÍÍß

ÀÊÊÓÌÓËßÖÈß È ÈÑÏÎËÜÇÎÂÀÍÈÅ ÊÎÍÄÅÍÑÀÒÀ  ÏÐÎÖÅÑÑÀÕ ÎÕËÀÆÄÅÍÈß ÖÈÊËÎÂÎÃÎ ÂÎÇÄÓÕÀ ÃÀÇÎÂÎÃÎ ÄÂÈÃÀÒÅËß ÒÐÈÃÅÍÅÐÀÖÈÎÍÍÎÉ ÓÑÒÀÍÎÂÊÈ ÀÂÒÎÍÎÌÍÎÃÎ ÝÍÅÐÃÎÎÁÅÑÏÅ×ÅÍÈß

8589
(5)

Êèñëèöûí À. Ï.

EMISSION INHOMOGENITY CONTROL OF THE THERMIONIC CÀTHODE WORKING SURFACE DURING EMISSION TESTS

ÊÎÍÒÐÎËÜ Å̲ѲÉÍί ÍÅÎÄÍÎвÄÍÎÑÒ² ÐÎÁÎ×ί ÏÎÂÅÐÕͲ ÒÅÐÌÎÊÀÒÎÄ²Â Ï²Ä ×ÀÑ Å̲ѲÉÍÈÕ ÂÈÏÐÎÁÓÂÀÍÜ

ÊÎÍÒÐÎËÜ ÝÌÈÑÑÈÎÍÍÎÉ ÍÅÎÄÍÎÐÎÄÍÎÑÒÈ ÐÀÁÎ×ÅÉ ÏÎÂÅÐÕÍÎÑÒÈ ÒÅÐÌÎÊÀÒÎÄÀ  ÏÐÎÖÅÑÑÅ ÝÌÈÑÑÈÎÍÍÛÕ ÈÑÏÛÒÀÍÈÉ

9095
(6)

Áîíäàðåíêî Ñ. Ã.,
Ãàáðèíåö Â. À.

Efficiency of Using Aluminum Hydride for Rocket-Space Engines Based on Pasty Propellant

ÅÔÅÊÒÈÂͲÑÒÜ ÂÈÊÎÐÈÑÒÀÍÍß Ã²ÄÐÈÄÓ ÀËÞÌ²Í²Þ ÄËß ÐÀÊÅÒÍÎ-ÊÎÑ̲×ÍÈÕ ÄÂÈÃÓͲ ÍÀ ÏÀÑÒÎÏÎIJÁÍÎÌÓ ÏÀËȲ

ÝÔÔÅÊÒÈÂÍÎÑÒÜ ÏÐÈÌÅÍÅÍÈß ÃÈÄÐÈÄÀ ÀËÞÌÈÍÈß ÄËß ÐÀÊÅÒÍÎ-ÊÎÑÌÈ×ÅÑÊÈÕ ÄÂÈÃÀÒÅËÅÉ ÍÀ ÏÀÑÒÎÎÁÐÀÇÍÎÌ ÒÎÏËÈÂÅ

96103
(8)

Èíôîðìàöèîííûå òåõíîëîãèè

Ôåäîðîâè÷ O. Å.,
Ëåùåíêî Þ. À.

MODELING AND OPTIMIZATION DEPTH QUALITY CONTROL WITH LIMITED RESOURCES OF ENTERPRISE OF AEROSPACE INDUSTRY

ÌÎÄÅËÞÂÀÍÍß ÒÀ ÎÏÒÈ̲ÇÀÖ²ß ÃËÈÁÈÍÈ ÊÎÍÒÐÎËÞ ßÊÎÑÒ²  ÓÌÎÂÀÕ ÎÁÌÅÆÅÍÎÑÒ² ÐÅÑÓÐѲ ϲÄÏÐȪÌÑÒ ÀÅÐÎÊÎÑ̲×Íί ÃÀËÓDz

ÌÎÄÅËÈÐÎÂÀÍÈÅ È ÎÏÒÈÌÈÇÀÖÈß ÃËÓÁÈÍÛ ÊÎÍÒÐÎËß ÊÀ×ÅÑÒÂÀ  ÓÑËÎÂÈßÕ ÎÃÐÀÍÈ×ÅÍÍÎÑÒÈ ÐÅÑÓÐÑΠÏÐÅÄÏÐÈßÒÈÉ ÀÝÐÎÊÎÑÌÈ×ÅÑÊÎÉ ÎÒÐÀÑËÈ

104–107
(4)

Áàáåíêî Þ. Â.

ESTIMATION FEATURES OF ADMINISTRATIVE PLANE MODIFICATIONS ECONOMIC EFFICIENCY ON THE PROJECT STAGE

ÎÑÎÁËÈÂÎÑÒ² ÎÖ²ÍÊÈ ÅÊÎÍÎ̲×Íί ÅÔÅÊÒÈÂÍÎÑÒ² ÌÎÄÈÔ²ÊÀÖ²É ÀÄ̲ͲÑÒÐÀÒÈÂÍÎÃΠ˲ÒÀÊÀ ÍÀ ÅÒÀϲ ¯Õ ÏÐÎÅÊÒÓÂÀÍÍß

ÎÑÎÁÅÍÍÎÑÒÈ ÎÖÅÍÊÈ ÝÊÎÍÎÌÈ×ÅÑÊÎÉ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÌÎÄÈÔÈÊÀÖÈÉ ÀÄÌÈÍÈÑÒÐÀÒÈÂÍÎÃÎ ÑÀÌÎËÅÒÀ ÍÀ ÝÒÀÏÅ ÈÕ ÏÐÎÅÊÒÈÐÎÂÀÍÈß

108–111
(4)

 

 

 

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- âõîäèò â óòâåðæäåííûé ÃÀÊ Ïåðå÷åíü íàó÷íûõ ïðîôåññèîíàëüíûõ èçäàíèé Óêðàèíû, â êîòîðûõ ìîãóò ïóáëèêîâàòüñÿ ðåçóëüòàòû äèññåðòàöèîííûõ ðàáîò íà ñîèñêàíèå ó÷åíûõ ñòåïåíåé äîêòîðà è êàíäèäàòà íàóê (ñì. ïðèêàç ÌÎÍ Óêðàèíû ¹1279 îò 6.11.2014 ã.);

ñîõðàíÿåòñÿ â îáùåãîñóäàðñòâåííîé ðåôåðàòèâíîé áàçå äàííûõ «Óêðà¿í³êà íàóêîâà» è ïóáëèêóåòñÿ â ñîîòâåòñòâóþùèõ òåìàòè÷åñêèõ ñåðèÿõ óêðàèíñêîãî ðåôåðàòèâíîãî æóðíàëà «Äæåðåëî» (ñâîáîäíûé îí-ëàéíîâûé äîñòóï ê ðåñóðñàì íà Web-ñåðâåðå http://www.nbuv.gov.ua) (Óêðàèíà),

ñîõðàíÿåòñÿ â ðåôåðàòèâíîé áàçå äàííûõ Âñåðîññèéñêîãî èíñòèòóòà íàó÷íîé è òåõíè÷åñêîé èíôîðìàöèè (ÂÈÍÈÒÈ) Ðîññèéñêîé àêàäåìèè íàóê è ïóáëèêóåòñÿ â ñîîòâåòñòâóþùèõ òåìàòè÷åñêèõ ñåðèÿõ ÐÆ (ñâîáîäíûé îí-ëàéíîâûé äîñòóï ê ðåñóðñàì íà Web-ñåðâåðå http://www.viniti.ru) (Ðîññèéñêàÿ Ôåäåðàöèÿ),

- âêëþ÷åí â ìåæäóíàðîäíûå áèáëèîìåòðè÷åñêèå è íàóêîìåòðè÷åñêèå áàçû äàííûõ: íàó÷íîé ýëåêòðîííîé áèáëèîòåêè eLIBRARY.RU (Ðîññèéñêàÿ Ôåäåðàöèÿ); Index Copernicus (ICV 2013: 4,83) (Ïîëüøà); CiteFactor; Google Scholar (áèáëèîìåòðè÷åñêèå ïîêàçàòåëèquot.=2096 / h = 10 / i10 = 15).