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

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ² ÒÅÕÍÎËÎòß. – 2015. – ¹ 5 (122). – 111 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2015. – ¹ 5 (122). – 111 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2015. – ¹ 5 (122). – 111 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

Ìèòèêîâ Þ. À.

APPROACH OF ROCKET ENGINE FUEL TANK HIGH TEMPRATURE PRESSURIZATION SYSTEM PARAMETER PHYSICAL MODELLING DURING ROCKET LAUNCH

ϲÄÕ²Ä ÄÎ Ô²ÇÈ×ÍÎÃÎ ÌÎÄÅËÞÂÀÍÍß ÏÀÐÀÌÅÒв ÑÈÑÒÅÌ ÍÀÄÄÓÂÀÍÍß ÏÀËÈÂÍÈÕ ÁÀʲ ÐÓØ²ÉÍÈÕ ÓÑÒÀÍÎÂÎÊ ÐÀÊÅÒ-ÍÎѲ¯Â

ÏÎÄÕÎÄ Ê ÔÈÇÈ×ÅÑÊÎÌÓ ÌÎÄÅËÈÐÎÂÀÍÈÞ ÏÀÐÀÌÅÒÐΠÑÈÑÒÅÌ ÂÛÑÎÊÎÒÅÌÏÅÐÀÒÓÐÍÎÃÎ ÍÀÄÄÓÂÀ ÒÎÏËÈÂÍÛÕ ÁÀÊΠÄÂÈÃÀÒÅËÜÍÛÕ ÓÑÒÀÍÎÂÎÊ ÏÐÈ ÑÒÀÐÒÅ ÐÀÊÅÒ-ÍÎÑÈÒÅËÅÉ

5–10
(6)

Íàçèí Â. È.

INFLUENCE OF DAMPING OF RESILIENT SETTING OF RINGS ON DISK ON DYNAMIC DESCRIPTIONS OF HYDROSTATODINAMIC BEARING OF THE DOUBLED TYPE

ÂÏËÈ ÄÅÌÏÔÓÂÀÍÍß ÏÐÓÆÍί ÓÑÒÀÍÎÂÊÈ Ê²ËÅÖÜ ÍÀ ÄÈÑÊÓ ÍÀ ÄÈÍÀ̲×Ͳ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ Ã²ÄÐÎÑÒÀÒÎÄÈÍÀ̲×ÍÎÃÎ Ï²ÄØÈÏÍÈÊÀ ÇÄÂΪÍÎÃÎ ÒÈÏÓ

ÂËÈßÍÈÅ ÄÅÌÏÔÈÐÎÂÀÍÈß ÓÏÐÓÃÎÉ ÓÑÒÀÍÎÂÊÈ ÊÎËÅÖ ÍÀ ÄÈÑÊÅ ÍÀ ÄÈÍÀÌÈ×ÅÑÊÈÅ ÕÀÐÀÊÒÅÐÈÑÒÈÊÈ ÃÈÄÐÎÑÒÀÒÎÄÈÍÀÌÈ×ÅÑÊÎÃÎ ÏÎÄØÈÏÍÈÊÀ ÑÄÂÎÅÍÍÎÃÎ ÒÈÏÀ

11–15
(5)

Ñåðåäà Â. À. 

OPTIMIZATION OF DYNAMIC CHARACTERISTICS OF GROUND CATAPULT WITH MULTISTAGE PNEUMATIC DRIVE

ÎÏÒÈ̲ÇÀÖ²ß ÄÈÍÀ̲×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÍÀÇÅÌÍί ÊÀÒÀÏÓËÜÒÈ Ç ÁÀÃÀÒÎÊÀÑÊÀÄÍÈÌ ÏÍÅÂÌÎÏÐÈÂÎÄÎÌ

ÎÏÒÈÌÈÇÀÖÈß ÄÈÍÀÌÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÍÀÇÅÌÍÎÉ ÊÀÒÀÏÓËÜÒÛ Ñ ÌÍÎÃÎÊÀÑÊÀÄÍÛÌ ÏÍÅÂÌÎÏÐÈÂÎÄÎÌ

16–20
(5)

Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ

Øèïóëü Î. Â.,
Êóçíåöîâ È. Á.,
Ïàëàçþê Å. C.

METHOD OF THE MODE SETTING DURING THERMAL-PULSE TREATMENT WITH THE REQUIREMENTS FOR EDGE QUALITY

ÌÅÒÎÄÈÊÀ ÏÐÈÇÍÀ×ÅÍÍß ÐÅÆÈ̲ ÒÅÐÌβÌÏÓËÜÑÍÎÃÎ ÎÏÎÐßÄÆÅÍÍß Ç ÓÐÀÕÓÂÀÍÍßÌ ÂÈÌÎà ÄÎ ßÊÎÑÒ² ÊÐÎÌÊÈ

ÌÅÒÎÄÈÊÀ ÍÀÇÍÀ×ÅÍÈß ÐÅÆÈÌΠÒÅÐÌÎÈÌÏÓËÜÑÍÎÉ ÎÒÄÅËÊÈ Ñ Ó×ÅÒÎÌ ÒÐÅÁÎÂÀÍÈÉ Ê ÊÀ×ÅÑÒÂÓ ÊÐÎÌÊÈ

21–26
(6)

Äåãòÿðåâ À. Â.,
Êàøàíîâ À. Ý.,
Ìàëàé÷óê Â. Ï.

CURRENT STATUS AND TASKS FOR SPACE ROCKETRY PRODUCTS NDT AND TECHNICAL DIAGNOSTICS UPGRADE

ÑÒÀÍ ÒÀ ÇÀÂÄÀÍÍß ÂÄÎÑÊÎÍÀËÅÍÍß ÌÅÒÎÄÎËÎò×ÍÈÕ ÎÑÍΠÍÅÐÓÉͲÂÍÎÃÎ ÊÎÍÒÐÎËÞ ÒÀ ÒÅÕͲ×Íί IJÀÃÍÎÑÒÈÊÈ ÐÀÊÅÒÍÎ-ÊÎÑ̲×Íί ÒÅÕͲÊÈ

ÑÎÑÒÎßÍÈÅ È ÇÀÄÀ×È ÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈß ÌÅÒÎÄÎËÎÃÈ×ÅÑÊÈÕ ÎÑÍΠÍÅÐÀÇÐÓØÀÞÙÅÃÎ ÊÎÍÒÐÎËß È ÒÅÕÍÈ×ÅÑÊÎÉ ÄÈÀÃÍÎÑÒÈÊÈ ÐÀÊÅÒÍÎ-ÊÎÑÌÈ×ÅÑÊÎÉ ÒÅÕÍÈÊÈ

27–34
(8)

ßêîâåíêî Â. Â.,
Êóøíèð Í. Â.

MATHEMATICAL MODEL OF THE RESIDUAL MAGNETIZATION OF THE FERROMAGNETIC PARTS OF THE LOCAL AREA

ÌÀÒÅÌÀÒÈ×ÍÀ ÌÎÄÅËÜ ÇÀËÈØÊÎÂί ÍÀÌÀÃͲ×ÅÍÎÑÒ² ËÎÊÀËÜÍί IJËßÍÊÈ ÔÅÐÎÌÀÃͲÒÍί ÄÅÒÀ˲

ÌÀÒÅÌÀÒÈ×ÅÑÊÀß ÌÎÄÅËÜ ÎÑÒÀÒÎ×ÍÎÉ ÍÀÌÀÃÍÈ×ÅÍÍÎÑÒÈ ËÎÊÀËÜÍÎÃÎ Ó×ÀÑÒÊÀ ÔÅÐÐÎÌÀÃÍÈÒÍÎÉ ÄÅÒÀËÈ

35–39
(5)

Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ

Betin A. V.,
Shakoori A.,
 Betin D. A.,
Mortazavi M.

ASSESSMENT INFLUENCE OF INCOMPLETE SIMILARITY OF DYNAMICALLY SCALED MODELS ON FLIGHT-TEST RESULTS

ÎÖ²ÍÊÀ ÂÏËÈÂÓ ÍÅÏÎÂÍί ÏÎIJÁÍÎÑÒ² ²ËÜÍÎ˲ÒÀÞ×ί ÌÎÄÅ˲ ÍÀ ÐÅÇÓËÜÒÀÒÈ ËÜÎÒÍÈÕ ÄÎÑË²ÄÆÅÍÜ

ÎÖÅÍÊÀ ÂËÈßÍÈß ÍÅÏÎËÍÎÃÎ ÏÎÄÎÁÈß ÑÂÎÁÎÄÍÎËÅÒÀÞÙÅÉ ÌÎÄÅËÈ ÍÀ ÐÅÇÓËÜÒÀÒÛ ËÅÒÍÛÕ ÈÑÑËÅÄÎÂÀÍÈÉ

40–47
(8)

Áëîõèí Ë. Í.,
Îñàä÷èé Ñ. È.

SYNTHESIS OF THE OPTIMIZED STRUCTURES OF REGULATORS FOR THE CONTROL SYSTEMS OF A MOVING OBJECT

ÑÈÍÒÅÇ ÎÏÒÈ̲ÇÎÂÀÍÈÕ ÑÒÐÓÊÒÓÐ ÐÅÃÓËßÒÎÐ²Â Ó ÑÈÑÒÅ̲ ÓÏÐÀÂ˲ÍÍß ÐÓÕÎÌÈÌ ÎÁ’ªÊÒÎÌ

ÑÈÍÒÅÇ ÎÏÒÈÌÈÇÈÐÎÂÀÍÍÛÕ ÑÒÐÓÊÒÓÐ ÐÅÃÓËßÒÎÐÎÂ Â ÑÈÑÒÅÌÅ ÓÏÐÀÂËÅÍÈß ÏÎÄÂÈÆÍÛÌ ÎÁÚÅÊÒÎÌ

48–53
(6)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Ôèëèïêîâñêèé Ñ. Â. 

NONLINEAR OSCILLATIONS OF A ROTOR OF COOLING TURBINE OF PLANE

ÍÅ˲ͲÉͲ ÊÎËÈÂÀÍÍß ÐÎÒÎÐÀ ÒÓÐÁÎÕÎËÎÄÈËÜÍÈÊÀ ˲ÒÀÊÀ

ÍÅËÈÍÅÉÍÛÅ ÊÎËÅÁÀÍÈß ÐÎÒÎÐÀ ÒÓÐÁÎÕÎËÎÄÈËÜÍÈÊÀ ÑÀÌÎ˨ÒÀ

54–60
(7)

Ðàä÷åíêî À. Í.,
Êàíòîð Ñ. À.

THE METHOD OF EVALUATION OF RATIONAL HEAT LOAD ON ABSORPTION-EJECTOR THERMOTRANSFORMER FOR COOLING REGENERATIVE GTU INTAKE AIR OF COMPRESSOR STATIONS

ÌÅÒÎÄ ÂÈÁÎÐÓ ÐÀÖ²ÎÍÀËÜÍÎÃÎ ÒÅÏËÎÂÎÃÎ ÍÀÂÀÍÒÀÆÅÍÍß ÀÁÑÎÐÁÖ²ÉÍÎ-ÅÆÅÊÒÎÐÍÎÃÎ ÒÅÐÌÎÒÐÀÍÑÔÎÐÌÀÒÎÐÀ ÎÕÎËÎÄÆÅÍÍß ÏβÒÐß ÍÀ ÂÕÎIJ ÐÅÃÅÍÅÐÀÒÈÂÍÈÕ ÃÒÓ ÊÎÌÏÐÅÑÎÐÍÈÕ ÑÒÀÍÖ²É

ÌÅÒÎÄ ÂÛÁÎÐÀ ÐÀÖÈÎÍÀËÜÍÎÉ ÒÅÏËÎÂÎÉ ÍÀÃÐÓÇÊÈ ÀÁÑÎÐÁÖÈÎÍÍÎ-ÝÆÅÊÒÎÐÍÎÃÎ ÒÅÐÌÎÒÐÀÍÑÔÎÐÌÀÒÎÐÀ ÎÕËÀÆÄÅÍÈß ÂÎÇÄÓÕÀ ÍÀ ÂÕÎÄÅ ÐÅÃÅÍÅÐÀÒÈÂÍÛÕ ÃÒÓ ÊÎÌÏÐÅÑÑÎÐÍÛÕ ÑÒÀÍÖÈÉ

61–64
(4)

Ðàä÷åíêî Ð. Í.,
Áîãäàíîâ Í. Ñ.,
Êàëèíè÷åíêî È. Â.

THE BASES OF RATIONAL DESIGNING OF SCAVENGE AIR COOLING SYSTEM WITH EJECTOR THERMOTRANSFORMER FOR MARINE LOW SPEED DIESEL ENGINE

ÎÑÍÎÂÈ ÐÀÖ²ÎÍÀËÜÍÎÃÎ ÏÐÎÅÊÒÓÂÀÍÍß ÑÈÑÒÅÌÈ ÎÕÎËÎÄÆÅÍÍß ÍÀÄÄÓÂÍÎÃÎ ÏβÒÐß ÑÓÄÍÎÂÎÃÎ ÌÀËÎÎÁÅÐÒÎÂÎÃÎ ÄÈÇÅËß ÅÆÅÊÒÎÐÍÈÌ ÒÅÐÌÎÒÐÀÍÑÔÎÐÌÀÒÎÐÎÌ

ÎÑÍÎÂÛ ÐÀÖÈÎÍÀËÜÍÎÃÎ ÏÐÎÅÊÒÈÐÎÂÀÍÈß ÑÈÑÒÅÌÛ ÎÕËÀÆÄÅÍÈß ÍÀÄÄÓÂÎ×ÍÎÃÎ ÂÎÇÄÓÕÀ ÑÓÄÎÂÎÃÎ ÌÀËÎÎÁÎÐÎÒÍÎÃÎ ÄÈÇÅËß ÝÆÅÊÒÎÐÍÛÌ ÒÅÐÌÎÒÐÀÍÑÔÎÐÌÀÒÎÐÎÌ

65–68
(4)

Äìèòð³ºâ Ñ. Î.,
Ïîïîâ Î. Â.,
ßêóøåíêî Î. Ñ.,
Ïîòàïîâ Â. ª.

METHODICAL BASIS OF DIAGNOSING TURBOFAN ENGINES WITH THE USE OF ARTIFICIAL INTELLIGENCE

ÌÅÒÎÄÈ×Ͳ ÎÑÍÎÂÈ Ä²ÀÃÍÎÑÒÓÂÀÍÍß ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÎÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÓÍÀ Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ ÇÀÑÎÁ²Â ØÒÓ×ÍÎÃÎ ²ÍÒÅËÅÊÒÓ

ÌÅÒÎÄÈ×ÅÑÊÈÅ ÎÑÍÎÂÛ ÄÈÀÃÍÎÑÒÈÐÎÂÀÍÈß ÒÓÐÁÎÐÅÀÊÒÈÂÍÎÃÎ ÄÂÓÕÊÎÍÒÓÐÍÎÃÎ ÄÂÈÃÀÒÅËß Ñ ÈÑÏÎËÜÇÎÂÀÍÈÅÌ ÑÐÅÄÑÒ ÈÑÊÓÑÑÒÂÅÍÍÎÃÎ ÈÍÒÅËËÅÊÒÀ

69–73
(5)

Èíôîðìàöèîííûå òåõíîëîãèè

Âîëîñþê Â. Ê.,
Âó Òà Êûîíã,

Òèìîùóê Å. Í. 

STATISTICAL SYNTHESIS OF RADIOMETRIC SYSTEM WITH N ANTENNA ARRAYS FOR DISTANCE ESTIMATION TO THE AREA OF SPATIALLY DISTRIBUTED OBJECT

ÑÒÀÒÈÑÒÈ×ÍÈÉ ÑÈÍÒÅÇ ÐÀIJÎÌÅÒÐÈ×Íί ÑÈÒÑÅÌÈ Ç N ÀÍÒÅÍÍÈÌÈ ÐÅØ²ÒÊÀÌÈ ÄËß ÂÈ̲ÐÞÂÀÍÍß ÄÀËÜÍÎÑÒ² ÄÎ ÇÀÄÀÍÎÃÎ ÅËÅÌÅÍÒÀ ÏÐÎÑÒÎÐÎÂÎ-ÐÎÇÏÎIJËÅÍÎÃÎ ÎÁ’ªÊÒÓ

ÑÒÀÒÈÑÒÈ×ÅÑÊÈÉ ÑÈÍÒÅÇ ÐÀÄÈÎÌÅÒÐÈ×ÅÑÊÎÉ ÑÈÑÒÅÌÛ Ñ N ÀÍÒÅÍÍÛÌÈ ÐÅØÅÒÊÀÌÈ ÄËß ÈÇÌÅÐÅÍÈß ÄÀËÜÍÎÑÒÈ ÄÎ ÇÀÄÀÍÍÎÃÎ Ó×ÀÑÒÊÀ ÏÐÎÑÒÐÀÍÑÒÂÅÍÍÎ-ÏÐÎÒ߯ÅÍÍÎÃÎ ÎÁÚÅÊÒÀ

74–79
(6)

Äóíàåâ Ä. Â.,
Êðèâîáîêîâ Ë. Â.

REGARDING COMPOSING COMPREHENSIVE DEVELOPMENT TEST PROGRAMS FOR INTEGRATED LAUNCH VEHICLE

ÄÎ ÏÈÒÀÍÍß ÑÒÂÎÐÅÍÍß ÊÎÌÏËÅÊÑÍί ÏÐÎÃÐÀÌÈ ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÃΠ²ÄÏÐÀÖÞÂÀÍÍß ÐÀÊÅÒ ÊÎÑ̲×ÍÎÃÎ ÏÐÈÇÀ×ÅÍÍß

Ê ÂÎÏÐÎÑÓ ÑÎÑÒÀÂËÅÍÈß ÊÎÌÏËÅÊÑÍÛÕ ÏÐÎÃÐÀÌÌ ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÉ ÎÒÐÀÁÎÒÊÈ ÐÀÊÅÒ ÊÎÑÌÈ×ÅÑÊÎÃÎ ÍÀÇÍÀ×ÅÍÈß

80–85
(6)

Áàðûøåâ È. Â.,
Ãîðáóíåíêî Î. À.,
Äàõíî À. À.

ERROR ANALYSIS OF POSITION LINE DETERMINATION USING SURFACES WITH VERTICAL GENERATRIX

ÀÍÀË²Ç ÏÎÕÈÁÎÊ ÂÈÇÍÀ×ÅÍÍß Ë²Í²É ÏÎËÎÆÅÍÍß ÏÐÈ ÂÈÊÎÐÈÑÒÀÍͲ ÏÎÂÅÐÕÎÍÜ Ç ÂÅÐÒÈÊÀËÜÍÎÞ Ò²ÐÍÎÞ

ÀÍÀËÈÇ ÏÎÃÐÅØÍÎÑÒÅÉ ÎÏÐÅÄÅËÅÍÈß ËÈÍÈÉ ÏÎËÎÆÅÍÈß ÏÐÈ ÈÑÏÎËÜÇÎÂÀÍÈÈ ÏÎÂÅÐÕÍÎÑÒÅÉ ÏÎËÎÆÅÍÈß Ñ ÂÅÐÒÈÊÀËÜÍÎÉ ÎÁÐÀÇÓÞÙÅÉ

86–91
(6)

Ïðîí÷àêîâ Þ. Ë.,
Ëåùåíêî Þ. À.

QUALITY ASSURANCE REQUIREMENTS IN THE CREATION OF GROWING ENTERPRISES

ÇÀÁÅÇÏÅ×ÅÍÍß ÂÈÌÎà ßÊÎÑÒ²  ÏÐÎÅÊÒÀÕ ÑÒÂÎÐÅÍÍß Ï²ÄÏÐȪÌÑÒÂÀ, ÙÎ ÐÎÇÂÈÂÀªÒÜÑß

ÎÁÅÑÏÅ×ÅÍÈÅ ÒÐÅÁÎÂÀÍÈÉ ÊÀ×ÅÑÒÂÀ ÏÐÎÈÇÂÎÄÑÒÂÀ ÂÛÑÎÊÎÒÅÕÍÎËÎÃÈ×ÅÑÊÎÉ ÏÐÎÄÓÊÖÈÈ Â ÏÐÎÅÊÒÀÕ ÌÎÄÅÐÍÈÇÀÖÈÈ ÐÀÇÂÈÂÀÞÙÅÃÎÑß ÏÐÅÄÏÐÈßÒÈ

92–98
(7)

Áàêóìåíêî Í. Ñ.

MODEL OF DISTANCE LEARNING FOR THE PREPARATION OF CIVIL AVIATION PILOTS

ÌÎÄÅËÜ ÑÈÑÒÅÌÈ ÄÈÑÒÀÍÖ²ÉÍÎÃÎ ÍÀÂ×ÀÍÍß ÄËß Ï²ÄÃÎÒÎÂÊÈ Ï²ËÎҲ ÖȲËÜÍί À²ÀÖ²¯

ÌÎÄÅËÜ ÑÈÑÒÅÌÛ ÄÈÑÒÀÍÖÈÎÍÍÎÃÎ ÎÁÓ×ÅÍÈß ÄËß ÏÎÄÃÎÒÎÂÊÈ ÏÈËÎÒΠÃÐÀÆÄÀÍÑÊÎÉ ÀÂÈÀÖÈÈ

99–103
(5)

Áàðàííèê Â. Â.,
Ðÿáóõà Þ. Í.

METHOD OF INTEGRITY OF VIDEOINFORMATION RESOURCES FOR THE TWO-CONCEPTUAL METHOD OF PROCESSING OF VIDEO FRAMES WITH IDENTIFICATION OF THEIR SEMANTIC LOADING

ÌÅÒÎÄ ÎÖ²ÍÊÈ Ö²Ë²ÑÍÎÑÒ² ²ÄÅβÍÔÎÐÌÀÖ²ÉÍÈÕ ÐÅÑÓÐѲ ÄËß ÄÂÎÕÊÎÍÖÅÏÒÓÀËÜÍÎÃÎ ÌÅÒÎÄÓ ÎÁÐÎÁÊÈ Â²ÄÅÎÊÀÄÐ²Â Ç ²ÄÅÍÒÈÔ²ÊÀÖ²ªÞ ¯Õ ÑÅÌÀÍÒÈ×Íί ÍÀÃÐÓÇÊÈ

ÌÅÒÎÄ ÎÖÅÍÊÈ ÖÅËÎÑÒÍÎÑÒÈ ÂÈÄÅÎÈÍÔÎÐÌÀÖÈÎÍÍÛÕ ÐÅÑÓÐÑΠÄËß ÄÂÓÕÊÎÍÖÅÏÒÓÀËÜÍÎÃÎ ÌÅÒÎÄÀ ÎÁÐÀÁÎÒÊÈ ÂÈÄÅÎÊÀÄÐÎÂ Ñ ÈÄÅÍÒÈÔÈÊÀÖÈÅÉ ÈÕ ÑÅÌÀÍÒÈ×ÅÑÊÎÉ ÍÀÃÐÓÇÊÈ

104–109
(6)

 

 

 

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Íàó÷íî-òåõíè÷åñêèé æóðíàë «Àâèàöèîííî-êîñìè÷åñêàÿ òåõíèêà è òåõíîëîãèÿ»

- 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.=2171 / h = 10 / i10 = 18).