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) |
Ñòðàíèöû (pages) |
||
English |
Óêðà¿íñüêà ìîâà |
Ðóññêèé
ÿçûê |
||
Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ
àïïàðàòîâ |
||||
Äîöåíêî
Â. Í., |
SIMPLIFIED dynamic model of
high-lift control system |
ÑÏÐÎÙÅÍÀ ÌÎÄÅËÜ ÑÈÑÒÅÌÈ ÊÅÐÓÂÀÍÍß ÇÀÊÐÈËÊÀÌÈ ² ÏÅÐÅÄÊÐÈËÊÀÌÈ |
ÓÏÐÎÙÅÍÍÀß ÌÎÄÅËÜ ÑÈÑÒÅÌÛ ÓÏÐÀÂËÅÍÈß ÇÀÊÐÛËÊÀÌÈ È ÏÐÅÄÊÐÛËÊÀÌÈ |
5–9 |
Äàâûäîâà
À. Â. |
EXPERIMENTAL
INVESTIGATIONS OF THE HYDRAULIC RESISTANCE COEFFICIENT OF THE MESH PHASES
DELIMITERS IN UNSTEADY LIQUID FLOW |
ÅÊÑÏÅÐÈÌÅÍÒÀËÜͲ ÄÎÑË²ÄÆÅÍÍß ÊÎÅÔ²Ö²ªÍÒÓ
òÄÐÀÂ˲×ÍÎÃÎ ÎÏÎÐÓ Ñ²Ò×ÀÑÒÈÕ
ÐÎÇIJËÞÂÀײ ÔÀÇ Â ÍÅÑÒÀÖ²ÎÍÀÐÍÎÌÓ
вÄÈÍÍÎÌÓ ÏÎÒÎÖ² |
10–15 |
|
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 |
16–25 |
Äóíàåâ
Ä. 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 |
26–31 |
|
Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è
óïðàâëåíèå ïîëåòîì ëåòàòåëüíûõ àïïàðàòîâ |
||||
Ñóááîòà
À. Ì., |
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» |
32–37 |
|
Ãåðãåëü
È. À., |
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 |
38–42 |
|
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 |
43–46 |
|
Ñâèðèäîâ Â. È., |
VIBRATION
DIAGNOSTICS ROLLING AND SLIDING BEARINGS |
²ÁÐÎIJÀÃÍÎÑÒÓÂÀÍÍß Ï²ÄØÈÏÍÈʲ ÊÎ×ÅÍÍß ÒÀ
ÊÎÂÇÀÍÍß |
47–53 |
|
Õàëàòîâ
À. À., |
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 |
54–59 |
|
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 |
60–64 |
Ìèòèêîâ
Þ. À., |
PROPULSION
SYSTEM TANK PRESSURIZATION WITH SOLID FUEL GAS PRODUCER EXPERIMENTAL STUDY |
ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÅ
ÄÎÑË²ÄÆÅÍÍß ÍÀÄÄÓÂÓ ÁÀʲ ÐÓØ²ÉÍÈÕ ÓÑÒÀÍÎÂÎÊ
ÒÂÅÐÄÎÏÀËÈÂÍÈÌÈ ÃÀÇÎÃÅÍÅÐÀÒÎÐÀÌ |
65–70 |
|
Ðàä÷åíêî Í. È., |
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 |
71–75 |
Ðàä÷åíêî À. Í., |
METODOLOGICAL APROACHES OF RATINAL DESIGNING
OF COMBINED WASTE HEAT RECOVERY SYSTEM FOR GAS
TURBINE UNIT INTAKE AIR COOLING |
ÌÅÒÎÄÎËÎò×ÍÈÉ
ϲÄÕ²Ä ÄÎ ÐÀÖ²ÎÍÀËÜÍÎÃÎ ÏÐÎÅÊÒÓÂÀÍÍß ÊÎÌÁ²ÍÎÂÀÍί ÒÅÏËÎÂÈÊÎÐÈÑÒÎÂÓÞ×ί
ÑÈÑÒÅÌÈ ÎÕÎËÎÄÆÅÍÍß ÏβÒÐß ÍÀ ÂÕÎIJ ÃÀÇÎÒÓÐÁ²ÍÍί ÓÑÒÀÍÎÂÊÈ |
76–79 |
|
Ðàä÷åíêî Ð. Í., |
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¯ |
80–84 |
|
Ðàä÷åíêî À. Í., |
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 |
85–89 |
|
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 |
90–95 |
Áîíäàðåíêî Ñ. Ã., |
Efficiency of Using Aluminum Hydride for
Rocket-Space Engines Based on Pasty Propellant |
ÅÔÅÊÒÈÂͲÑÒÜ ÂÈÊÎÐÈÑÒÀÍÍß
òÄÐÈÄÓ ÀËÞÌ²Í²Þ ÄËß ÐÀÊÅÒÍÎ-ÊÎÑ̲×ÍÈÕ ÄÂÈÃÓͲ ÍÀ ÏÀÑÒÎÏÎIJÁÍÎÌÓ ÏÀËȲ |
96–103 |
|
Èíôîðìàöèîííûå òåõíîëîãèè |
||||
Ôåäîðîâè÷ O. Å., |
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 |
104–107 |
|
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 |
108–111 |
Óâàæàåìûå ÷èòàòåëè!
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 ïîêàçàòåëè – quot.=2096 / h = 10 / i10 = 15).