Íàöèîíàëüíûé
àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé
èíñòèòóò”
ISSN
1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ²
ÒÅÕÍÎËÎòß. – 2012. – ¹ 3(90). – 118 ñ.
ISSN
1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2012. – ¹ 3(90). –
118 ñ.
ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2012. – ¹ 3(90). – 118 p.
ÑÒÀÒÜè (articleS)
Àâòîðû |
Íàçâàíèå ñòàòüè
(article title) |
Ñòðàíèöû (pages) |
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English |
Óêðà¿íñüêà ìîâà |
Ðóññêèé
ÿçûê |
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Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ |
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Æäàíîâ È.À. |
SIMULATION OF PIPE BENDING UNDER COMBINED LOADING |
ÌÎÄÅËÞÂÀÍÍß
ÏÐÎÖÅѲ ÇÃÈÍÀÍÍß ÒÐÓÁ  ÓÌÎÂÀÕ ÊÎÌÁ²ÍÎÂÀÍÎÃÎ
ÍÀÂÀÍÒÀÆÅÍÍß |
ÌÎÄÅËÈÐÎÂÀÍÈÅ
ÏÐÎÖÅÑÑÎÂ ÃÈÁÊÈ ÒÐÓÁ Â ÓÑËÎÂÈßÕ ÊÎÌÁÈÍÈÐÎÂÀÍÍÎÃÎ ÍÀÃÐÓÆÅÍÈß |
5–9 |
Êîâàëåíêî Â.À. |
RESEARCHING OF
DEFECTS RESULTING IN PRODUCTION AGGREGATES OF ROCKET AND SPACE TECHNOLOGY
MADE OF POLYMERIC COMPOSITE MATERIALS REPORT 1. TOLERANCE OF MOLDED PRODUCTS
THICKNESS FROM PROJECT VALUE |
ÄÎÑË²ÄÆÅÍÍß ÒÅÕÍÎËÎò×ÍÈÕ ÄÅÔÅÊÒ²Â, ÙÎ ÂÈÍÈÊÀÞÒÜ Ó ÂÈÐÎÁÍÈÖÒ² ÀÃÐÅÃÀÒ²Â
ÐÀÊÅÒÍÎ-ÊÎÑ̲×Íî¿ ÒÅÕͲÊè Ç ÏÎ˲ÌÅÐÍÈÕ ÊÎÌÏÎÇÈÖ²ÉÍÈÕ ÌÀÒÅвÀ˲Â.
ÏβÄÎÌËÅÍÍß 1. ÄÎÏÓÑÊÈ ÍÀ ²ÄÕÈËÅÍÍß Â²Ä ÏÐÎÅÊÒÍÎÃÎ ÇÍÀ×ÅÍÍß ÒÎÂÙÈÍÈ ÂÈÐÎÁÓ,
ÙÎ ÔÎÐÌÓªÒÜÑß |
10–21 |
|
Æóíü Ã.Ã. |
ACCELERATION OF
STABILIZATION OF TEMPERATURE FIELD IN A CRYOVESSEL |
ÏÐÈÑÊÎÐÅÍÍß ÑÒÀÁ²Ë²ÇÀÖ²¯ ÒÅÌÏÅÐÀÒÓÐÍÎÃÎ
ÏÎËß Â ÊвÎÏÎÑÓIJ |
22–25 |
|
Íåæâåä³ëîâ À.Þ. |
A MODEL OF
DIFFUZION SATURATION |
ÌÎÄÅËÜ ÏÐÎÖÅÑÑÀ
ÄÈÔÔÓÇÈÎÍÍÎÃÎ ÍÀÑÛÙÅÍÈß |
26–29 |
|
Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ
àïïàðàòîâ |
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Ìèòèêîâ Þ.À., |
WAYS FOR IMPROVING RELIABILITI AND SAFETY
IN USAGE OF ROCKET COMPLEX |
ØËßÕÈ Ï²ÄÂÈÙÅÍÍß ÍÀIJÉÍÎÑÒ² ² ÁÅÇÏÅÊÈ
ÅÊÑÏËÓÀÒÀÖ²¯ ÐÀÊÅÒÍÈÕ ÊÎÌÏËÅÊѲ |
ÏÓÒÈ ÏÎÂÛØÅÍÈß
ÍÀĨÆÍÎÑÒÈ È ÁÅÇÎÏÀÑÍÎÑÒÈ ÝÊÑÏËÓÀÒÀÖÈÈ ÐÀÊÅÒÍÛÕ ÊÎÌÏËÅÊÑΠ|
30–36 |
Zosimovych N.V., |
INFLUENCE OF FACTORS DETERMINE THE VALUE OF TOLERANCE ON
THE OUTBOARD SIDE UNMANNED AERIAL VEHICLES |
ÂËÈßÍÈÅ ÔÀÊÒÎÐÎÂ, ÎÏÐÅÄÅËßÞÙÈÕ ÂÅËÈ×ÈÍÓ
ÄÎÏÓÑÊÀ ÍÀ ÂÍÅØÍÈÅ ÎÁÂÎÄÛ ÁÅÑÏÈËÎÒÍÛÕ ËÅÒÀÒÅËÜÍÛÕ ÀÏÏÀÐÀÒÎÂ
|
ÂÏËÈ ÔÀÊÒÎÐIÂ, ßÊI ÂÈÇÍÀ×ÀÞÒÜ ÇÍÀ×ÅÍÍß
ÄÎÏÓÑÊÓ ÍÀ ÇÎÂÍIØÍI ÎÁÐÈÑÈ ÁÅÇÏIËÎÒÍÈÕ ËIÒÀËÜÍÈÕ ÀÏÀÐÀҲ |
37–46 |
Êèñëèöûí À.Ï., |
TEMPERATURE DISTRIBUTION ALONG THE ACTIVE LAYER OF THE OXIDE CATHODE
UNDER THE CONTINUOUS AND PULSE CURRENT TAKE-OFFS |
ÐÎÇÏÎÄ²Ë ÒÅÌÏÅÐÀÒÓÐÈ Ó ÀÊÒÈÂÍÎÌÓ
ØÀв ÎÊÑÈÄÍÎÃÎ ÊÀÒÎÄÀ ÏÐÈ
ÁÅÇÏÅÐÅÐÂÍÎÌÓ ÒÀ ²ÌÏÓËÜÑÍÎÌÓ ÑÒÐÓÌβÄÁÎÐÀÕ |
ÐÀÑÏÐÅÄÅËÅÍÈÅ
ÒÅÌÏÅÐÀÒÓÐÛ Â ÀÊÒÈÂÍÎÌ ÑËÎÅ ÎÊÑÈÄÍÎÃÎ ÊÀÒÎÄÀ ÏÐÈ ÍÅÏÐÅÐÛÂÍÎÌ È ÈÌÏÓËÜÑÍÎÌ ÒÎÊÎÎÒÁÎÐÀÕ |
47–55 |
Àýðîäèíàìèêà, äèíàìèêà, áàëëèñòèêà è
óïðàâëåíèå ïîëåòîì |
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Ôèðñîâ Ñ.Í., |
CONTROLS FOR A SMALL-SIZED vertical takeoff and landing AIRCRAFT DURING TRANSIENT
FROM ONE FLIGHT CONDITION TO ANOTHER |
ÓÏÐÀÂ˲ÍÍß
ÌÀËÎÃÀÁÀËÈÒÍÈÌ Ë²ÒÀËÜÍÈÌ ÀÏÀÐÀÒÎÌ ÂÅÐÒÈÊÀËÜÍÎÃÎ ÇËÜÎÒÓ ÒÀ ÏÎÑÀÄÊÈ ÏÐÈ
ÏÅÐÅղIJ Â²Ä ÎÄÍÎÃÎ ÐÅÆÈÌÓ ÏÎËÜÎÒÓ Â ²ÍØÈÉ |
56–61 |
|
Ñïåñèâöåâ Â.Â. |
RESEARCHING OF
INTERNAL FLOWS IN SUPERSONIC JET |
ÄÎÑË²ÄÆÅÍÍß ÂÍÓÒÐÅØÍ²Õ ÏËÈͲÂ
ÍÀÄÇÂÓÊÎÂÎÃÎ ÑÒÐÓÌÅÍß |
62–67 |
|
Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ
ëåòàòåëüíûõ àïïàðàòîâ |
||||
Ëîãèíîâ Â.Â., |
means to improve the battle trainer aircraft performance
characteristics by replacing the propulsion engine |
ØËßÕÈ Ïîêðàùåííÿ ËüîÒÍÎ-ÒÅÕͳ÷íÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ íàâ÷àëüÍÎ-ÁÎÉÎÂîãî
ë³òàêà ÍÀ ÎÑÍγ ÇÀ̳Íè ÄÂÈÃóíà ñèëîâî¿ óñòàíîâêè |
68–75 |
|
Ãîöóëåíêî Â.Â., |
THE INDEPENDENCE OF OSCILLATIONS OF THE RIJKE PHENOMENON OF HYPOTHESES RAYLEIGH AND HEY DYNAMIC DAMPING |
ùîäÎ ÍÅÇÀËÅÆÍÎÑÒ² ÀÂÒÎÊÎËÈÂÀÍÜ ÔÅÍÎÌÅÍÓ Ð²ÉÊÅ Â²Ä ÓÌΠòÏÎÒÅÇÈ ÐÅËÅß ÒÀ ¯Õ ÄÈÍÀ̲×ÍÅ ÄÅÌÏÔ²ÐÓÂÀÍÍß |
76–81 |
|
×èãðèí Â.Ñ., |
RESEARCH POSSIBILITY USE OF THE INDUCTION GAUGE FREQUENCY OF ROTATION
FOR ANALYSIS UNBALANCE OF ROTOR’S JET ENGINES |
ÄÎÑË²ÄÆÅÍÍß ÌÎÆËÈÂÎÑÒ² ÂÈÊÎÐÈÑÒÀÍÍß ²ÍÄÓÊÖ²ÉÍÎÃÎ ÄÀÒ×ÈÊÀ ×ÀÑÒÎÒÈ ÎÁÅÐÒÀÍÍß
ÄËß ÀÍÀ˲ÇÀ ÄÈÑÁÀËÀÍÑÓ ÐÎÒÎÐÀ ÃÒÄ |
82–88 |
|
Äàâèäîâ À.Î. |
THE THEORETICAL
DESCRIPTION AND ANALYSIS OF THE MECHANISMS OF DEGRADATION PROCESSES IN
ELECTROCHEMICAL BATTERIES FOR USE IN OBJECTS OF SPACE-ROCKET HARDWARE |
ÒÅÎÐÅÒÈ×ÍÈÉ ÎÏÈÑ ÒÀ ÀÍÀË²Ç ÌÅÕÀͲÇ̲Â
ÏÐÎÒ²ÊÀÍÍß ÄÅÃÐÀÄÀÖ²ÉÍÈÕ ÏÐÎÖÅѲ  ÅËÅÊÒÐÎղ̲×ÍÈÕ ÀÊÓÌÓËßÒÎÐÀÕ ÏÐÈ ¯Õ ÂÈÊÎÐÈÑÒÀÍͲ
 ÎÁ’ªÊÒÀÕ ÐÀÊÅÒÍÎ-ÊÎÑ̲×Íί ÒÅÕͲÊÈ |
89–98 |
|
Èíôîðìàöèîííûå òåõíîëîãèè |
||||
Çåìëÿ÷åíêî À.Í., |
AUTOMATIC IMAGE
COMPRESSION FOR SIGNAL-DEPENDENT NOISE IN THE NEIGHBORHOOD OF OPTIMAL
OPERATION POINT |
ÀÂÒÎÌÀÒÈ×ÍÅ ÑÒÈÑÍÅÍÍß ÇÎÁÐÀÆÅÍÜ
ÏÐÈ ÑÈÃÍÀËÜÍÎ-ÇÀËÅÆÍÈÕ ÇÀÂÀÄÀÕ Â ÎÊÎËÈÖ² ÎÏÒÈÌÀËÜÍί ÐÎÁÎ×ί ÒÎ×ÊÈ |
99–107 |
|
Êîçóá À.Ì.,
|
OPTIMIZATION
SET OF OPTICAL-ELECTRONIC SURVEILLANCE FOR AEROSPACE MONITORING FOREST |
ÎÏÒÈÌÈÇÀÖÈß ÊÎÌÏËÅÊÒÀ
ÑÐÅÄÑÒ ÎÏÒÈÊÎ-ÝËÅÊÒÐÎÍÍÎÃÎ ÍÀÁËÞÄÅÍÈß ÄËß ÀÝÐÎÊÎÑÌÈ×ÅÑÊÎÃÎ ÌÎÍÈÒÎÐÈÍÃÀ
ËÅÑÍÛÕ ÌÀÑÑÈÂ |
108–112 |
|
Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè
ïðåäïðèÿòèÿìè, |
||||
Êðàñíèêîâ Â.Í., |
RISK MANAGEMENT OF COMPLEX PROJECTS AEROSPACE INDUSTRY |
ÓÏÐÀÂ˲ÍÍß ÐÈÇÈÊÀÌÈ ÑÊËÀÄÍÈÕ ÏÐÎÅÊÒ²Â
À²ÀÖ²ÉÍÎ-ÊÎÑ̲×Íί ÃÀËÓDz |
ÓÏÐÀÂËÅÍÈß
ÐÈÑÊÀÌÈ ÑËÎÆÍÛÕ ÏÐÎÅÊÒΠÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÎÉ ÎÒÐÀÑËÈ |
113–116 |
Óâàæàåìûå ÷èòàòåëè!
Íàó÷íî-òåõíè÷åñêèé æóðíàë “ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß
ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß“
âêëþ÷åí â ïåðå÷åíü íàó÷íûõ èçäàíèé, â
êîòîðûõ ìîãóò ïóáëèêîâàòüñÿ îñíîâíûå ðåçóëüòàòû äèññåðòàöèîííûõ ðàáîò (ñì.
ïîñòàíîâëåíèå ïðåçèäèóìà ÂÀÊ Óêðàèíû ¹1-05/4 îò 14.10.2009ã)
Ðåôåðàòèâíàÿ èíôîðìàöèÿ ñîõðàíÿåòñÿ:
– â
îáùåãîñóäàðñòâåííîé ðåôåðàòèâíîé áàçå äàííûõ «Óêðà¿í³êà
íàóêîâà» è ïóáëèêóåòñÿ â ñîîòâåòñòâóþùèõ òåìàòè÷åñêèõ
ñåðèÿõ ÓÐÆ «Äæåðåëî» (ñâîáîäíûé îí-ëàéíîâûé äîñòóï ê ðåñóðñàì íà Web-ñåðâåðå http://www.nbuv.gov.ua),
– 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).