Íàöèîíàëüíûé
àýðîêîñìè÷åñêèé óíèâåðñèòåò èì. Í.Å. Æóêîâñêîãî “Õàðüêîâñêèé àâèàöèîííûé
èíñòèòóò”
ISSN
1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ ²
ÒÅÕÍÎËÎòß. – 2012. – ¹ 9(96). – 274 ñ.
ISSN
1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2012. – ¹ 9(96). –
274 ñ.
ISSN
1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2012. – ¹ 9(96). – 274 p.
ÑÒÀÒÜè (articleS)
Àâòîðû |
Íàçâàíèå ñòàòüè
(article title) |
Ñòðàíèöû(pages) |
||
English |
Óêðà¿íñüêà
ìîâà |
Ðóññêèé
ÿçûê |
||
Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ |
||||
Êàëèíèíà Í.Å., |
TECHNOLOGICAL PROPERTIES
OF MODIFIED CASTINGS SILUMINS |
ÒÅÕÍÎËÎò×Ͳ
ÂËÀÑÒÈÂÎÑÒ² ÌÎÄÈÔ²ÊÎÂÀÍÈÕ ËÈÂÀÐÍÈÕ ÑÈËÓ̲Ͳ |
ÒÅÕÍÎËÎÃÈ×ÅÑÊÈÅ
ÑÂÎÉÑÒÂÀ ÌÎÄÈÔÈÖÈÐÎÂÀÍÍÛÕ ËÈÒÅÉÍÛÕ ÑÈËÓÌÈÍÎÂ |
7–10 |
Êðèâöîâ Â.Ñ., |
PROBLEMS OF
SPLINE INTERPOLATION WITH SMOOTHLY-LIMITED
KINEMATICAL PARAMETERS OF MOVEMENT IN TASKS OF CNC HIGH-SPEED
EQUIPMENT |
ÏÐÎÁËÅÌÈ
ÑÏËÀÉÍÎÂî¿ ²ÍÒÅÐÏÎËßÖ²¯ ²Ç ÃËÀÄÊÎ-ÎÁÌÅÆÅÍÈÌÈ Ê²ÍÅÌÀÒÈ×ÍÈÌÈ ÏÀÐÀÌÅÒÐÀÌÈ ÐÓÕÓ â
ÇÀÄÀ×ÀÕ ×ÈÑËÎÂÎÃÎ ÏÐÎÃÐÀÌÍÎÃÎ ÊÅÐÓÂÀÍÍß ÂÈÑÎÊÎØÂÈÄʲÑÍÈÌ ÓÑÒÀÒÊÓÂÀÍÍßÌ |
11–19 |
|
Òðåòüÿê Â.Â. |
COMPUTATION OF PARAMETERS OF MAGNETIC-IMPULSIVE STAMPING IN OBJECTIVE
PRESENTATION |
ÐÎÇÐÀÕÓÍÎÊ
ÏÀÐÀÌÅÒв ÌÀÃͲÒÍÎ-²ÌÏÓËÜÑÍÎÃÎ ØÒÀÌÏÓÂÀÍÍß Â ÎÁ'ªÊÒÍÎÌÓ ÓßÂËÅÍͲ |
ÐÀÑ×ÅÒ ÏÀÐÀÌÅÒÐÎÂ
ÌÀÃÍÈÒÍÎ-ÈÌÏÓËÜÑÍÎÉ ØÒÀÌÏÎÂÊÈ Â ÎÁÚÅÊÒÍÎÌ ÏÐÅÄÑÒÀÂËÅÍÈÈ |
20–24 |
Äðàãîáåöêèé Â.Â., |
DM OF
ECOLOGICAL SAFETY DURING REALIZATION OF TECHNOLOGIES OF COLD SPRAYING OF DETAILS OF TURBO-ENGINES OF ËÅÒÅËÜÍÛÕ
VEHICLES |
ÇÀÁÅÇÏÅ×ÅÍÍß ÅÊÎËÎò×Íί
ÁÅÇÏÅÊÈ ÏÐÈ ÐÅÀ˲ÇÀÖ²¯ ÒÅÕÍÎËÎÃ²É ÕÎËÎÄÍÎÃÎ ÍÀÏÈËÅÍÍß ÄÅÒÀËÅÉ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ
ÄÂÈÃÓͲ ˲ÒÀËÜÍÈÕ ÀÏÀÐÀҲ |
25–28 |
|
Êîâàëü÷óê È.À., |
PROSPECTS
OF THE USE SPRUTEXPRO FOR DEVELOPMENT OF CONSTRUCTION AND TECHNOLOGY OF MAKING PURVEYANCES BY
IMPULSIVE TECHNOLOGIES |
ÏÅÐÑÏÅÊÒÈÂÈ
ÂÈÊÎÐÈÑÒÎÂÓÂÀÍÍß SPRUTEXPRO ÄËß ÐÎÇÐÎÁÊÈ ÊÎÍÑÒÐÓÊÖ²¯ ² ÒÅÕÍÎËÎò¯ ÂÈÃÎÒÎÂËÅÍÍß
ÏÎÊÎÂÎÊ ÇÀ ÄÎÏÎÌÎÃÎÞ ²ÌÏÓËÜÑÍÈÕ
ÒÅÕÍÎËÎÃ²É |
29–33 |
|
Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ
ëåòàòåëüíûõ àïïàðàòîâ |
||||
Ëîãèíîâ Â.Â., |
Analyses of aerodynamic parameters of
regional passenger airplane with different TFE in the system of power plant |
äîñë³äæåííÿ àåðîäèíàì³÷íèõ õàðàêòåðèñòèê ðåã³îíàëüíîãî òðàíñïîðòíîãî ë³òàêà ç ð³çíèìè ÒÐÄÄ â ñèñòåì³ ñèëîâî¿
óñòàíîâêè |
34–39 |
|
Òàðàñîâ À.È., |
PROBLEMS OF CREATION PULSE DETONATION GAS TURBINE ENGINES |
ÏÐÎÁËÅÌÈ
ÑÒÂÎÐÅÍÍß ÃÀÇÎÒÓÐÁIÍÍÎÃÎ ÏÓËÜÑÓÞ×ÅÃÎ ÄÅÒÎÍÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ |
ÏÐÎÁËÅÌÛ ÑÎÇÄÀÍÈß
ÃÀÇÎÒÓÐÁÈÍÍÎÃÎ ÏÓËÜÑÈÐÓÞÙÅÃÎ ÄÅÒÎÍÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß |
40–44 |
Êðàéíþê À.È. |
PRE-CONDITIONS OF
CREATION OF DISK ENGINE REACTIVE ROTATIONS OF CASCADE EXCHANGE PRESSURE |
ÏÅÐÅÄÓÌÎÂÈ ÑÒÂÎÐÅÍÍß ÄÈÑÊÎÂÎÃÎ ÄÂÈÃÓÍÀ
ÐÅÀÊÒÈÂÍÎÃÎ ÎÁÅÐÒÀÍÍß
ÊÀÑÊÀÄÍÎÃÎ ÎÁ̲ÍÓ ÒÈÑÊÎÌ |
ÏÐÅÄÏÎÑÛËÊÈ
ÑÎÇÄÀÍÈß ÄÈÑÊÎÂÎÃÎ ÄÂÈÃÀÒÅËß ÐÅÀÊÒÈÂÍÎÃÎ ÂÐÀÙÅÍÈß ÊÀÑÊÀÄÍÎÃÎ ÎÁÌÅÍÀ ÄÀÂËÅÍÈÅÌ
|
45–48 |
Øåðåìåòüåâ À.Â. |
CONSTRUCTIVE
SIMULARITY OF THE AVIATION GTE PARTS |
ÊÎÍÑÒÐÓÊÒÈÂÍÀ ÏÎIJÁͲÑÒÜ Ó ÄÅÒÀËßÕ
À²ÀÖ²ÉÍÈÕ ÃÒÄ |
49–53 |
|
Òèíÿêîâ Ä.Â., |
AnalysIs oN Tapered wing shapes of partial criteria of their
effectiveness |
ÀÍÀË²Ç ÃÅÎÌÅÒÐÈ×ÍÈÕ ÔÎÐÌ
ÒÐÀÏÅÖ²ªÏÎIJÁÍÈÕ ÊÐÈË ÇÀ ×ÀÑÒÈÍÍÈÌÈ
ÊÐÈÒÅвßÌÈ ¯Õ ÅÔÅÊÒÈÂÍÎÑÒ² |
ÀÍÀËÈÇ ÔÎÐÌ
ÒÐÀÏÅÖÈÅÂÈÄÍÛÕ ÊÐÛËÜÅ ÏÎ ×ÀÑÒÍÛÌ ÊÐÈÒÅÐÈßÌ ÈÕ ÝÔÔÅÊÒÈÂÍÎÑÒÈ |
54–60 |
Ñòåïàíåíêî Ñ.Ì., |
ROLE OF OUTSOURCING IN THE SYSTEM OF PROCESSES FOR CREATING NEW AERO
ENGINE SPECIMENS |
ÐÎËÜ ÀÓÒÑÎÐÑÈÍÃÓ Â ÑÈÑÒÅ̲ ÏÐÎÖÅѲ ÑÒÂÎÐÅÍÍß ÍÎÂÈÕ ÇÐÀÇʲ À²ÀÖ²ÉÍÈÕ ÄÂÈÃÓͲ |
ÐÎËÜ ÀÓÒÑÎÐÑÈÍÃÀ
 ÑÈÑÒÅÌÅ ÏÐÎÖÅÑÑΠÑÎÇÄÀÍÈß ÍÎÂÛÕ ÎÁÐÀÇÖΠÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ |
61–65 |
Áóãàåíêî Î.Ì. |
SIMULATION OF
JOINT WORK PROGRAM AND THREE-PHASE ACCELERATION GTE NOZZLE |
ÏÐÎÃÐÀÌÀ ÌÎÄÅËÞÂÀÍÍß
ÑÓ̲ÑÍί ÐÎÁÎÒÈ ÃÒÄ ÒÀ ÒÐÈÔÀÇÎÂÎÃÎ ÐÎÇòÍÍÎÃÎ ÑÎÏËÀ |
ÏÐÎÃÐÀÌÌÀ
ÌÎÄÅËÈÐÎÂÀÍÈß ÑÎÂÌÅÑÒÍÎÉ ÐÀÁÎÒÛ ÃÒÄ È ÒÐÅÕÔÀÇÍÎÃÎ ÐÀÇÃÎÍÍÎÃÎ ÑÎÏËÀ |
66–70 |
Ãðèçóí Ì.Í., |
CALCULATION OF TWO-DIMENSIONAL
INVISCID FLOWS WITH NEWTON METHOD |
ÐÎÇÐÀÕÓÍÎÊ ÄÂÎÂÈ̲ÐÍÈÕ ÍÅÂ’ßÇÊÈÕ
ÒÅ×²É ÇÀ ÄÎÏÎÌÎÃÎÞ ÌÅÒÎÄÀ ÍÜÞÒÎÍÀ |
71–75 |
|
Ñûñîåâ Þ.À. |
FEATURES OF CREATION OF SYSTEMS FOR
HIGH-PRECISION GAS MIXING |
ÎÑÎÁËÈÂÎÑÒ² ÑÒÂÎÐÅÍÍß ÃÀÇÎÇ̲ØÓÞ×ÈÕ
ÑÈÑÒÅÌ Ï²ÄÂÈÙÅÍί ÒÎ×ÍÎÑÒ² |
ÎÑÎÁÅÍÍÎÑÒÈ
ÑÎÇÄÀÍÈß ÃÀÇÎÑÌÅØÈÂÀÞÙÈÕ ÑÈÑÒÅÌ ÏÎÂÛØÅÍÍÎÉ ÒÎ×ÍÎÑÒÈ |
76–80 |
Äîëìàòîâ Ä.À. |
SINGLE
HYDROCARBON DROP COMBUSTION IN THE PRESENCE OF STATIONARY ARC |
ÃÎвÍÍß ÎÄÈÍÎÊί ÊÐÀÏ˲ ÂÓÃËÅÂÎÄÍÅÂÎÃÎ
ÏÀËÈÂÀ Ó ÏÐÈÑÓÒÍÎÑÒ² ÑÒÀÖ²ÎÍÀÐÍÎÃÎ
ÐÎÇÐßÄÓ |
ÃÎÐÅÍÈÅ
ÎÄÈÍÎ×ÍÎÉ ÊÀÏËÈ ÓÃËÅÂÎÄÎÐÎÄÍÎÃÎ ÒÎÏËÈÂÀ  ÏÐÈÑÓÒÑÒÂÈÈ ÑÒÀÖÈÎÍÀÐÍÎÃÎ ÐÀÇÐßÄÀ |
81–86 |
Ñîòíèêîâ Â.Ï. |
MULTIPROCESSOR
APPROXIMATION OF GAS ISOTHERMIC COMPRESSION |
ÌÓËÜÒÈÏÐÎÖÅÑÍÀ ÀÏÐÎÊÑÈÌÀÖ²ß
²ÇÎÒÅÐ̲×ÍÎÃÎ ÑÒÈÑÊÀÍÍß ÃÀÇÓ |
87–92 |
|
Ãàéäà÷óê À.Â., |
CONCEPTION OF
OPTIMIZATION OF APPLICATION OF COMPOSITION MATERIALS TAKING INTO ACCOUNT
ECONOMIC EFFICIENCY |
ÊÎÍÖÅÏÖ²ß ÎÏÒÈ̲ÇÀÖ²¯ ÇÀÑÒÎÑÓÂÀÍÍß
ÊÎÌÏÎÇÈÖ²ÉÍÈÕ ÌÀÒÅвÀË²Â Ç ÓÐÀÕÓÂÀÍÍßÌ
ÅÊÎÍÎ̲×Íί ÅÔÅÊÒÈÂÍÎÑÒ² |
ÊÎÍÖÅÏÖÈß
ÎÏÒÈÌÈÇÀÖÈÈ ÊÎÍÑÒÐÓÊÖÈÉ ÈÇ ÊÎÌÏÎÇÈÖÈÎÍÍÛÕ ÌÀÒÅÐÈÀËÎÂ Ñ Ó×ÅÒÎÌ ÝÊÎÍÎÌÈ×ÅÑÊÎÉ
ÝÔÔÅÊÒÈÂÍÎÑÒÈ |
93–98 |
Íàçèí Â.È. |
RESEARCH OF
CAPACITY OF HYDROSTATICAL BEARING OF HOB TYPE |
ÄÎÑË²ÄÆÅÍÍß
ÏÐÀÖÅÇÄÀÒÍÎÑÒ² òÄÐÎÑÒÀÒÈ×ÍÎÃÎ
Ï²ÄØÈÏÍÈÊÀ ÂÒÓËÊÎÂÎÃÎ ÒÈÏÀ |
ÈÑÑËÅÄÎÂÀÍÈÅ
ÐÀÁÎÒÎÑÏÎÑÎÁÍÎÑÒÈ ÃÈÄÐÎÑÒÀÒÈ×ÅÑÊÎÃÎ ÏÎÄØÈÏÍÈÊÀ ÂÒÓËÎ×ÍÎÃÎ ÒÈÏÀ |
99–104 |
Ãîëîùàïîâ Â.Í., |
Òhe management of thermal state of high-power turbine
cylinders according to the changing of radial gaps |
ÓÏÐÀÂ˳Ííÿ ÒÅÏËÎÂèÌ Ñòàíîì ÖÈ˳ÍÄг òóðá³íè âåëèêî¿ ïîòóæíîñò³ çà Ç̳íîþ
ÐÀijÀËÜÍèÕ ÇÀÇÎг |
ÓÏÐÀÂËÅÍÈÅ ÒÅÏËÎÂÛÌ
ÑÎÑÒÎßÍÈÅÌ ÖÈËÈÍÄÐΠÒÓÐÁÈÍÛ ÁÎËÜØÎÉ ÌÎÙÍÎÑÒÈ ÏÎ ÈÇÌÅÍÅÍÈÞ ÐÀÄÈÀËÜÍÛÕ ÇÀÇÎÐÎÂ
|
105–108 |
Åâäîêèìåíêî Þ.È., |
STRUCTURE AND PROPERTIES OF THE NICKEL COATINGS RECEIVED FROM NOT FUSED PARTICLES BY HIGH-VELOCITY AIR-FUEL SPRAYING |
ÑÒÐÓÊÒÓÐÀ ² ÂËÀÑÒÈÂÎÑÒ² ͲÊÅËÅÂÈÕ
ÏÎÊÐÈÒÒ²Â, ÎÒÐÈÌÀÍÈÕ Ç ÍÅÐÎÇÏËÀÂËÅÍÈÕ
×ÀÑÒÈÍÎÊ ÂÈÑÎÊÎØÂÈÄʲÑÍÈÌ
ÏβÒÐßÍÎ-ÏÀËÈÂÍÈÌ ÍÀÏÈËÅÍÍßÌ |
109–114 |
|
Ñíåæíîé Ã.Â., |
The magnetic state of AUSTENITIC MATRIX AND MECHANICAL PROPERTIES
high-manganese steel |
Ìàãí²òíÈÉ ñÒÀÍ
àóñòåí²òíî¯ ìàòðèö² ² ìåõàí²÷Ͳ ÂËÀÑÒÈÂÎÑÒ² âÈñîêîìàÍÃÀÍÎÂÈÕ ÊÐÈÖÜ |
ÌÀÃÍÈÒÍÎÅ
ÑÎÑÒÎßÍÈÅ ÀÓÑÒÅÍÈÒÍÎÉ ÌÀÒÐÈÖÛ È ÌÅÕÀÍÈ×ÅÑÊÈÅ ÑÂÎÉÑÒÂÀ ÂÛÑÎÊÎÌÀÐÃÀÍÖÅÂÛÕ
ÑÒÀËÅÉ |
115–120 |
Ïîâãîðîäíèé Â.Î. |
The determinanion
of the thermomechanical characteristics including solution invers problem of
thermoelasticity |
Âèçíà÷åííÿ
òåðìîìåõàí³÷íèõ õàðàêòåðèñòèê ìàòåð³àë³â
íà îñíîâ³ ðîçâ’ÿçêó îáåðíåíèõ çàäà÷ òåðìîïðóæíîñò³ |
121–126 |
|
Âåäü Â.Å., |
HEAT-RESISTANT COATING FOR GTE TURBINE
BLADES |
ÆÀÐÎÑÒ²ÉÊÅ ÏÎÊÐÈÒÒß ÄËß ËÎÏÀÒÎÊ ÒÓÐÁ²Í
ÃÒÄ |
127–131 |
|
Çèíüêîâñêèé À.Ï., |
INFLUENCE OF
DISSIPATION OF ENERGY IN MATERIAL ON VIBRATIONS OF STRUCTURAL ELEMENTS WITH
NONUNIFORMITIES |
Âïëèâ
ðîçñ³þâàííÿ åíåð㳿 â ìàòåð³àë³ íà êîëèâàííÿ
êîíñòðóêòèâíèõ åëåìåíò³â ç íåîäíîð³äíîñòÿìè |
ÂËÈßÍÈÅ ÐÀÑÑÅßÍÈß
ÝÍÅÐÃÈÈ Â ÌÀÒÅÐÈÀËÅ ÍÀ ÊÎËÅÁÀÍÈß ËÎÏÀÒÎÊ Ñ ÍÅÎÄÍÎÐÎÄÍÎÑÒßÌÈ |
132–137 |
Êàðà÷óí Â.Â., |
CYCLIC AND AXIS NON-SYMMATRICAL COVER
DEFORMATION IN THE ACOUSTIC FIELD |
ÖÈÊ˲×ÍÀ ² ÎÑÅÍÅÑÈÌÅÒÐÈ×ÍÀ ÄÅÔÎÐÌÀÖ²ß
ÎÁÎËÎÍÊÈ Â ÀÊÓÑÒÈ×ÍÎÌÓ ÏÎ˲ |
ÖÈÊËÈ×ÅÑÊÀß È
ÎÑÅÍÅÑÈÌÌÅÒÐÈ×ÍÀß ÄÅÔÎÐÌÀÖÈß ÎÁÎËÎ×ÊÈ Â ÀÊÓÑÒÈ×ÅÑÊÎÌ ÏÎËÅ |
138–141 |
Õîðîëüñêèé Ï.Ã., |
TO SELECTION OF
THE LAUNCH VEHICLE FOR INJECTION TO THE INITIAL ORBITDEBRIS collector space vehicle |
ÄÎ ÂÈÁÎÐÓ ÐÀÊÅÒÈ-ÍÎÑ²ß ÄËß ÄÎÑÒÀÂÊÈ ÍÀ
ÂÈÕ²ÄÍÓ ÎÐÁ²ÒÓÑ̲ÒÒªÇÁÈÐÀËÜÍÎÃÎ ÊÎÑ̲×ÍÎÃÎ ÀÏÀÐÀÒÀ |
Ê
ÂÛÁÎÐÓ ÐÀÊÅÒÛ-ÍÎÑÈÒÅËß ÄËß ÄÎÑÒÀÂÊÈ ÍÀ ÈÑÕÎÄÍÓÞ ÎÐÁÈÒÓ ÌÓÑÎÐÎÑÎÁÈÐÀÞÙÅÃÎ
ÊÎÑÌÈ×ÅÑÊÎÃÎ ÀÏÏÀÐÀÒÀ |
142–145 |
Çàäîíöåâ Â.À. |
TWO
LIVES AND TWO ROCKETS OF WERNER VON BRAUN (1912-1977). TO THE 100TH ANNIVERSARY OF
HIS BIRTH |
ÄÂÀ ÆÈÒÒß ÒÀ IJ ÐÀÊÅÒÈ ÂÅÐÍÅÐÀ ÔÎÍ
ÁÐÀÓÍÀ (1912-1977). ÄÎ 100-в××ß ²Ç ÄÍß ÍÀÐÎÆÄÅÍÍß |
ÄÂÅ ÆÈÇÍÈ È ÄÂÅ
ÐÀÊÅÒÛ ÂÅÐÍÅÐÀ ÔÎÍ ÁÐÀÓÍÀ (1912-1977). Ê 100-ËÅÒÈÞ ÑÎ ÄÍß ÐÎÆÄÅÍÈß |
146–158 |
Ðåâà Â.Ñ., |
JUSTIFICATION
FOR PRODUCTION AND ELECTRIC POWER QUALITY CONTROL SYSTEM STRUCTURE AS PART OF
GROUND COMPLEX POWER SUPPLY SYSTEM |
ÎÁ¥ÐÓÍÒÓÂÀÍÍß ÍÅÎÁÕ²ÄÍÎÑÒ²
ÑÒÂÎÐÅÍÍß ² ÑÒÐÓÊÒÓÐÀ ÑÈÑÒÅÌÈ ÊÎÍÒÐÎËÞ ßÊÎÑÒ² ÅËÅÊÒÐÎÅÍÅÐò¯ Ó ÑÊËÀIJ ÑÈÑÒÅÌÈ ÅËÅÊÒÐÎÏÎÑÒÀ×ÀÍÍß ÍÀÇÅÌÍÎÃÎ ÊÎÌÏËÅÊÑÓ |
159–162 |
|
Êîíîõ Â.È., |
The FEATURES
OF MATHEMATICAL MODELING OF WORKING PROCESSES IN HYDRAULIC POWER systems WITH a PNEUMATIC ACTUATOR |
Îñîáëèâîñò³ ìàòåìàòè÷íîãî ìîäåëþâàííÿ ðîáî÷èõ ïðîöåñ³â â ÄÆÅÐÅËÀÕ Ã²äðàâë³÷íî¿ ïîòóæíîñò³ ç ïíåâìàòè÷íèì ïîâ³äíèêîì |
163–168 |
|
Êîâàëåíêî À.Í., |
Rated evaluation of factors that affect the gas-dynamic launch during high-altitude engine test |
ÐÎÇÐÀÕÓÍÊÎÂÀ
ÎÖ²ÍÊÀ ÔÀÊÒÎв ÙÎ ÂÏËÈÂÀÞÒÜ ÍÀ ÇÀÏÓÑÊ
ãàçîäèíàì³÷íî¿ òðóáè Ï²Ä ×ÀÑ ÂÈÏÐÎÁÓÂÀÍÍß ÂÈÑÎÒÍÎÃÎ ÄÂÈÃÓÍÀ |
169–173 |
|
Èâ÷åíêî Ë.Ô., |
EXPERIENCE OF DESIGNING OF THE autonomous
TURBINE TPU ENGINE RD861K |
ÄÎÑÂ²Ä ÏÐÎÅÊÒÓÂÀÍÍß ÀÂÒÎÍÎÌÍί ÒÓÐÁ²ÍÈ
ÒÍÀ ÄÂÈÃÓÍÀ ÐÄ861Ê |
174–179 |
|
Ïîìèí Î.Â., |
EXPERIENCE OF THE
ENTERPRISE FOR CLEARING INTERNAL HEAT-SHIELDING COVERING ROCKET ENGINES OF
FIRM FUEL AFTER THE WORK TERMINATION AT CARRYING OUT OF BENCH TESTS |
Äîñâ³ä
ï³äïðèºìñòâà ïî ãàñ³ííþ âíóòð³øíüîãî òåïëîçàõèñíîãî ïîêðèòòÿ ðàêåòíèõ äâèãóí³â òâåðäîãî ïàëèâà
ï³ñëÿ çàê³í÷åííÿ ðîáîòè ïðè ïðîâåäåíí³
ñòåíäîâèõ âèïðîáóâàíü |
180–184 |
|
Äàâèäîâ À.Î. |
THE ACADEMIC
QUESTIONS OF PROLONGATION OF LIFE TIME OF ELECTROCHEMICAL BATTERIES IN POWER
INSTALLATIONS OF SPACE-ROCKET OBJECTS |
ÎÑÍÎÂͲ ÅÒÀÏÈ ÄÎÑË²ÄÆÅÍÜ ÏÎ
ÇÀÁÅÇÏÅ×ÅÍÍÞ ÒÐÈÂÀËÎÃÎ ÐÅÑÓÐÑÓ
ÅËÅÊÒÐÎղ̲×ÍÈÕ ÀÊÓÌÓËßÒÎв  ÅÍÅÐÃÎÓÑÒÀÍÎÂÊÀÕ ÐÀÊÅÒÍÎ-ÊÎÑ̲×ÍÈÕ ÎÁ’ªÊҲ |
185–190 |
|
Öàãëîâ À.È. |
PLUME PARAMETERS
INVESTIGATION OF ELECTRODELESS ELECTRIC PROULSION THRUSTER WITH RF IONSZATION
OF WORKING MEDIUM |
ÄÎÑË²ÄÆÅÍÍß ÏÀÐÀÌÅÒв ÑÒÐÓ¯
ÁÅÇÅËÅÊÒÐÎÄÍÎÃÎ ÅÐÄ Ç Â× ²ÎͲÇÀÖ²ªÞ ÐÒ |
ÈÑÑËÅÄÎÂÀÍÈÅ
ÏÀÐÀÌÅÒÐΠÑÒÐÓÈ ÁÅÇÝËÅÊÒÐÎÄÍÎÃÎ ÝÐÄ Ñ Â× ÈÎÍÈÇÀÖÈÅÉ ÐÒ |
191–195 |
Òèòîâ Ì. Þ., |
Ions speed measuring in plasma beam of low-power Hall Effect thruster
SPT-20M using laser-induced fluorescence velocimetry |
ÂÈ̲РØÂÈÄÊÎÑÒÅÉ ²ÎͲ Â
Ïëàçìîâîìó ïó÷êó Õîëëîâñüêîãî ÄÂÈÃÓÍÀ
ÌÀËί ÏÎÒÓÆÍÎÑÒ² ÑÏÄ-20Ì ÌÅÒÎÄÎÌ ËÀÇÅÐÍÎ-³íäóêîâàíî¿ ôëóîðåñöåíö³¿ |
ÈÇÌÅÐÅÍÈÅ
ÑÊÎÐÎÑÒÅÉ ÈÎÍÎÂ Â ÏËÀÇÌÅÍÍÎÉ ÑÒÐÓÅ
ÕÎËËÎÂÑÊÎÃÎ ÄÂÈÃÀÒÅËß ÌÀËÎÉ ÌÎÙÍÎÑÒÈ ÑÏÄ-20Ì ÌÅÒÎÄÎÌ
ËÀÇÅÐÍÎ-ÈÍÄÓÖÈÐÎÂÀÍÍÎÉ ÔËÓÎÐÅÑÖÅÍÖÈÈ |
196–200 |
Àãååâà Å.Ã., |
EXPERIMENTALLY RESEARCH OF SELFHEATED HOLLOW CATHODE EROSION BY OPTICAL
SPECTROSCOPY METHOD |
ÅÊÑÏÅÐÈÌÅÍÒÀËÜÍÅ ÄÎÑË²ÄÆÅÍÍß ÅÐÎDz¯ ÁÅÇÍÀ×ÀËÜÍÎÃÎ ÏÎÐÎÆÍÈÑÒÎÃÎ ÊÀÒÎÄÀ
ÌÅÒÎÄÎÌ ÎÏÒÈ×Íί Å̲ѲÉÍί ÑÏÅÊÒÐÎÑÊÎϲ¯ |
201–205 |
|
Õèòüêî À.Â., |
HOLLOW CATHODES OF ELECTRIC PROPULSION NON-CLASSICAL SCHEMES |
ÏÎÐÎÆÍÈÑÒ² ÊÀÒÎÄÈ ÅËÅÊÒÐÈ×ÍÈÕ ÐÀÊÅÒÍÈÕ
ÄÂÈÃÓͲÂÍÅÊËÀÑÈ×Íί ÑÕÅÌÈ |
ÏÎËÛÅ ÊÀÒÎÄÛ
ÝËÅÊÒÐÈ×ÅÑÊÈÕ ÐÀÊÅÒÍÛÕ ÄÂÈÃÀÒÅËÅÉ ÍÅÊËÀÑÑÈ×ÅÑÊÎÉ ÑÕÅÌÛ |
206–209 |
×åðêóí À.Ì. |
RESEARCH METHOD OF PLASMA DOUBLE LAYER INFLUENCE ON HOLLOW CATHODE’S
GAS EFFICIENCY |
ÌÅÒÎÄÈÊÀ ÄÎÑË²ÄÆÅÍÍß ÂÏËÈÂÓ ÏÎIJÉÍÎÃÎ
ÏËÀÇÌÎÂÎÃÎ ØÀÐÓ ÍÀ ÃÀÇÎÂÓ ÅÔÅÊÒÈÂͲÑÒÜ
ÏÎÐÎÆÍÈÍÍÎÃÎ ÊÀÒÎÄÀ |
ÌÅÒÎÄÈÊÀ
ÈÑÑËÅÄÎÂÀÍÈß ÂËÈßÍÈß ÄÂÎÉÍÎÃÎ ÏËÀÇÌÅÍÍÎÃÎ ÑËÎß ÍÀ ÃÀÇÎÂÓÞ ÝÔÔÅÊÒÈÂÍÎÑÒÜ
ÏÎËÎÃÎ ÊÀÒÎÄÀ |
210–213 |
Óìàíñêèé À.Ï., |
STEEL HARDENING
BY ELECTRIC-SPARK ALLOYING WITH COMPOSITE MATERIALS OF TiB2-(Fe-Mo)
SYSTEM |
ÅËÅÊÒÐβÑÊÐÎÂÅ Ç̲ÖÍÅÍÍß ÑÒÀ˲ ÊÎÌÏÎÇÈÖ²ÉÍÈÌÈ ÌÀÒÅвÀËÀÌÈ ÑÈÑÒÅÌÈ TiB2-(Fe-Mo)
|
ÝËÅÊÒÐÎÈÑÊÐÎÂÎÅ
ÓÏÐÎ×ÍÅÍÈÅ ÑÒÀËÈ ÊÎÌÏÎÇÈÖÈÎÍÍÛÌÈ ÌÀÒÅÐÈÀËÀÌÈ ÑÈÑÒÅÌÛ TiB2-(Fe-Mo)
|
214–218 |
Á³ëÿêîâè÷ Î.Ì., |
RESEARCH OF
LUBRICATION EFFECT EFFECIENCY OF THE TRANSMISSION OILS IN THE CONDITIONS OF
THE PROTRACTED EXPLOITATION AT STATIONARE MODES OF FRICTION |
ÈÑÑËÅÄÎÂÀÍÈÅ ÝÔÅÊÒÈÂÍÎÑÒÈ ÑÌÀÇÛÂÀÞÙÅÃÎ
ÄÅÉÑÒÂÈß |
219–223 |
|
Ðÿáêîâ Â.È., |
SUPERSYMMETRIC
MODEL IN RESEARCH OF MATTER PROPERTIES |
CÓÏÅÐÑÈÌÅÒÐÈ×ÍÀ ÌÎÄÅËÜ Ó ÄÎÑË²ÄÆÅÍͲ
ÂËÀÑÒÈÂÎÑÒÅÉ ÐÅ×ÎÂÈÍÈ |
224–228 |
|
Èíôîðìàöèîííûå òåõíîëîãèè |
||||
Ìèðãîðîä Â.Ô., |
METHODS OF NUMERICAL REALIZATION OF
MATHEMATICAL MODELS OF DYNAMICAL PROCESSES IN THE FORM OF INTEGRAL EQUATION |
ÌÅÒÎÄÈ ×ÈÑÅËÜÍί ÐÅÀ˲ÇÀÖ²¯ ÌÀÒÅÌÀÒÈ×ÍÈÕ ÌÎÄÅËÅÉ ÄÈÍÀ̲×ÍÈÕ ÏÐîÖÅѲÂ
Ó ÔÎÐ̲ ²ÍÒÅÃÐÀËÜÍÈÕ Ð²ÂÍßÍÜ |
229–233 |
|
Åïèôàíîâ Ñ.Â., |
CREATING A
QUICK PROCEEDING MATHEMATICAL MODEL OF A TURBOSHAFT ENGINE STARTING
SIMULATION FOR AUTOMATIC CONTROL SYSTEM SYNTHESIS PURPOSES |
ÑÒÂÎÐÅÍÍß ØÂÈÄÊÎÐÀÕ²ÂÍί ÌÀÒÅÌÀÒÈ×Íί
ÌÎÄÅ˲ ÒÓÐÁÎÂÀËÜÍÎÃÎ ÄÂÈÃÓÍÀ ÍÀ ÅÒÀϲ
ÇÀÏÓÑÊÓ ÄËß Ð²ØÅÍÍß ÇÀÄÀ× ÑÈÍÒÅÇÓ
ÑÈÑÒÅÌ ÀÂÒÎÌÀÒÈ×ÍÎÃÎ ÊÅÐÓÂÀÍÍß |
234–242 |
|
Òàðàñåíêî À.È., |
full-range
dynamic GTE model |
øèðîêîäèàïàçîííà
ÄÈÍÀ̲÷íà ìîäåëü ãòä |
243–247 |
|
Ìàðàâèëëà Ýððåðà Ê. |
ANALYSIS OF THE
EFFECTIVESS OF ALTERNATIVE MODELS TO PREDICT THE COEFFICIENTS OF HEAT
EXCHANGE ON THE BLADE EXTERNAL SURFACE TAKING I NTO ACCONT THE ENGINE
IDIVIDUAL CHARACTERISTICS |
àíàë³ç
åôåêòèâíîñò³ ÷îòèðüîõ ð³çíèõ ìîäåëåé
äëÿ âèçíà÷åííÿ êîåô³ö³ºíò³â òåïëîâ³ääà÷³ íà çîâí³øí²é ïîâåðõí³ ëîïàòêè ç
ÓÐÀÕóÂÀÍÍßÌ âïëèâó ³íäèâ³äóàëüíèõ
õàðàêòåðèñòèê äâèãóí³â |
248–252 |
|
Âàñèëåíêî À.È., |
FORMING OF
CHANNELS FAILURE CRITERION FOR MEASURING GAS TURBINE ENGINE PARAMETERS AND
ACS RESPONSE |
ÔÎÐÌÓÂÀÍÍß ÎÇÍÀÊ
²ÄÌÎÂÈ ÊÀÍÀ˲ ÂÈ̲ÐÞÂÀÍÍß ÏÀÐÀÌÅÒвÂ
ÃÀÇÎÒÓÐÁ²ÍÍÎÃÎ ÄÂÈÃÓÍÀ ² ÐÅÀÊÖ²¯ ÍÀ ÍÜÎÃÎ ÑÀÊ ³ Ð ÀÃÐÅÃÀÒÓ |
253–256 |
|
Áóðàó Í.È., |
SIMULATION OF
THE TWO-LEVELS VIBRATION CONTROL SYSTEM OF AVIATION ENGINE BY USING NI LABVIEW TECHNIQUE |
ÌÎÄÅËÞÂÀÍÍß ÄÂÎвÂÍÅÂί ÑÈÑÒÅÌÈ
ÊÎÍÒÐÎËÞ Â²ÁÐÀÖ²¯ À²ÀÖ²ÉÍÎÃÎ
ÄÂÈÃÓÍÀ  ÑÈÑÒÅ̲ NI LABVIEW |
ÌÎÄÅËÈÐÎÂÀÍÈÅ ÄÂÓÕÓÐÎÂÍÅÂÎÉ
ÑÈÑÒÅÌÛ ÊÎÍÒÐÎËß ÂÈÁÐÀÖÈÈ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß Â ÑÈÑÒÅÌÅ NI LABVIEW |
257–262 |
Èíôîðìàöèîííûå òåõíîëîãèè â óïðàâëåíèè
ïðåäïðèÿòèÿìè, ïðîãðàììàìè è ïðîåêòàìè |
||||
Øîñòàê È.Â., |
AUTOMATION OF
PROCESS FORMING SHEDULED OF LESSONS BASED ON THE TENSOR IN TRAINING COMPLEX |
ÀÂÒÎÌÀÒÈÇÀÖ²ß ÏÐÎÖÅÑÓ ÑÊËÀÄÀÍÍß
ÐÎÇÊËÀÄÓ ÇÀÍßÒÜ ÍÀ ÎÑÍβ
ÒÅÍÇÎÐÍÎÃÎ ÎÁ×ÈÑËÅÍÍß Â Ó×ÁÎÂÎÌÓ ÊÎÌÏËÅÊѲ |
263–266 |
|
Ïîòàïîâà Ì.Â. |
SYSTEM MODEL OF
SCHEDULING OF PROGRAM PROJECTS |
ÑÈÑÒÅÌÍÀ ÌÎÄÅËÜ ÊÀËÅÍÄÀÐÍÎÃÎ ÏËÀÍÓÂÀÍÍß
ÏÐÎÃÐÀÌÍÈÕ ÏÐÎÅÊҲ |
ÑÈÑÒÅÌÍÀß ÌÎÄÅËÜ
ÊÀËÅÍÄÀÐÍÎÃÎ ÏËÀÍÈÐÎÂÀÍÈß ÏÐÎÃÐÀÌÌÍÛÕ ÏÐÎÅÊÒÎÂ |
267–272 |
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).