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

 

 

ISSN 1727-7337. À²ÀÖ²ÉÍÎ-ÊÎÑ̲×ÍÀ ÒÅÕͲÊÀ  ² ÒÅÕÍÎËÎòß. – 2013. – ¹ 9(106). – 286 ñ.

ISSN 1727-7337. ÀÂÈÀÖÈÎÍÍÎ-ÊÎÑÌÈ×ÅÑÊÀß ÒÅÕÍÈÊÀ È ÒÅÕÍÎËÎÃÈß. – 2013. – ¹ 9(106). – 286 ñ.

ISSN 1727-7337. AEROSPACE TECHNIC AND TECHNOLOGY. – 2013. – ¹ 9(106). – 286 ñ.

 

ÑÒÀÒÜè (articleS)

 

Àâòîðû
(ÿçûê
îðèãèíàëà)

Íàçâàíèå ñòàòüè  (article title)

Ñòðàíèöû

(pages)

English

Óêðà¿íñüêà ìîâà

Ðóññêèé ÿçûê

Òåõíîëîãèÿ ïðîèçâîäñòâà ëåòàòåëüíûõ àïïàðàòîâ

Ñîðîêèí Â.Ô.,
Êîìáàðîâ Â.Â.,
Òåðíþê È.À.

METHOD OF DIRECT STABILIZATION OF CONTOUR FEEDRATE FOR THE SPLINE INTERPOLATOR CNC SYSTEM

ÌÅÒÎÄ ÏÐßÌί ÑÒÀÁ²Ë²ÇÀÖ²¯ ÊÎÍÒÓÐÍί ØÂÈÄÊÎÑÒ² ÄËß ÑÏËÀÉÍÎÂîÃÎ ²ÍÒÅÐÏÎËßÒÎÐà ÑÈÑÒÅÌè ×ÏÓ

ÌÅÒÎÄ ÏÐßÌÎÉ ÑÒÀÁÈËÈÇÀÖÈÈ ÊÎÍÒÓÐÍÎÉ ÑÊÎÐÎÑÒÈ ÄËß ÑÏËÀÉÍÎÂÎÃÎ ÈÍÒÅÐÏÎËßÒÎÐÀ ÑÈÑÒÅÌÛ ×ÏÓ

7–13
(
7)

Ïðîåêòèðîâàíèå àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Çàäîíöåâ Â.À.

HERO OF SOCIALISTIC LABOR IVAN IVANOVYCH IVANOV (1918-1999) – THE FIRST CHIEF DESIGNER OF ENGINE DESIGN OFFICE KB-4 OF OKB-586 / YUZHNOYE DESIGN BUREAU

ÃÅÐÎÉ ÑÎÖ²À˲ÑÒÈ×Íί ÏÐÀÖ² ²ÂÀÍ ²ÂÀÍÎÂÈ× ²ÂÀÍΠ(1918-1999) – ÏÅÐØÈÉ ÃÎËÎÂÍÈÉ  ÊÎÍÑÒÐÓÊÒÎÐ ÄÂÈÃÓÍÍÎÃÎ ÊÁ-4 ÎÊÁ-586/ ÊÁ «ÞÆÍΪ»

ÃÅÐÎÉ ÑÎÖÈÀËÈÑÒÈ×ÅÑÊÎÃÎ ÒÐÓÄÀ ÈÂÀÍ ÈÂÀÍÎÂÈ× ÈÂÀÍΠ(1918-1999) – ÏÅÐÂÛÉ ÃËÀÂÍÛÉ ÊÎÍÑÒÐÓÊÒÎÐ ÄÂÈÃÀÒÅËÜÍÎÃÎ ÊÁ-4 ÎÊÁ-586/ÊÁ «ÞÆÍÎÅ»

14–24
(
11)

Äåãòÿðåâ À.Â.,
Äåãòÿðåâà Å.À.,
Íîâèêîâ À.Â.,
Òàòàðåâñêèé Ê.Ý.

ZENITH-3SL ILV LAUNCH DYNAMICS ANALYSIS from sea launch platform

Ðåçóëüòàòè àíàë²çó Äèíàì²êè ñòàðòó ÐÊÏ «ÇåíIò-3SL» ç ìîðñüêί ñòàðòîâî¯ ïëàòôîðìÈ, ùî çíàõîäèòüñÿ íà ïëàâó

ÐÅÇÓËÜÒÀÒÛ ÀÍÀËÈÇÀ ÄÈÍÀÌÈÊÈ ÑÒÀÐÒÀ ÐÊÍ «ÇÅÍÈÒ-3SL» Ñ ÍÀÕÎÄßÙÅÉÑß ÍÀ ÏËÀÂÓ ÌÎÐÑÊÎÉ ÑÒÀÐÒÎÂÎÉ ÏËÀÒÔÎÐÌÛ

25–31
(
7)

Äðîíü Í.Ì.,
Õîðîëüñêèé Ï.Ã.,
Äóáîâèê Ë.Ã.

FORECASTING OF CHARACTERISTICS OF THE SPECIALIZED SPACECRAFT  FOR THE GATHERING SMALL SPACE DEBRIS

ÏÐÎÃÍÎÇÓÂÀÍÍß ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÑÏÅÖ²À˲ÇÎÂÀÍÎÃÎ ÊÎÑ̲×ÍÎÃÎ ÀÏÀÐÀÒÀ ÄËß ÇÁÈÐÀÍÍß ÄвÁÍÎÃÎ ÊÎÑ̲×ÍÎÃÎ Ñ̲ÒÒß

ÏÐÎÃÍÎÇÈÐÎÂÀÍÈÅ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÑÏÅÖÈÀËÈÇÈÐÎÂÀÍÍÎÃÎ ÊÎÑÌÈ×ÅÑÊÎÃÎ ÀÏÏÀÐÀÒÀ ÄËß ÑÁÎÐÀ ÌÅËÊÎÃÎ ÊÎÑÌÈ×ÅÑÊÎÃÎ ÌÓÑÎÐÀ

32–37
(
6)

Êóøíèðåíêî C.È.,
Øåâöîâ Â.Å.

POSSIBILITY ANALYSIS OF USING DIFFERENT KINDS OF THE SPACECRAFT PROPULSION SYSTEMS FOR STRUGGLE AGAINST POLLUTION OF OUTER SPACE

ÀÍÀË²Ç ÌÎÆËÈÂÎÑÒ² ÂÈÊÎÐÈÑÒÀÍÍß Ð²ÇÍÈÕ ÒÈϲ ÄÂÈÃÓÍÍÈÕ ÓÑÒÀÍÎÂÎÊ ÄËß ÁÎÐÎÒÜÁÈ ²Ç ÇÀÑ̲×ÅÍÍßÌ ÊÎÑ̲×ÍÎÃÎ ÏÐÎÑÒÎÐÓ

ÀÍÀËÈÇ ÂÎÇÌÎÆÍÎÑÒÈ ÈÑÏÎËÜÇÎÂÀÍÈß ÐÀÇËÈ×ÍÛÕ ÒÈÏΠÄÂÈÃÀÒÅËÜÍÛÕ ÓÑÒÀÍÎÂÎÊ ÄËß ÁÎÐÜÁÛ Ñ ÇÀÑÎÐÅÍÈÅÌ ÊÎÑÌÈ×ÅÑÊÎÃÎ ÏÐÎÑÒÐÀÍÑÒÂÀ

38–42
(
5)

Íèêîëàåâ À.Ä.,
Áåëåöêèé À.Ñ.

AN INTERACTION OF CAVITATION SURGE OSCILLATIONS AND LONGITUDINAL OSCILLATIONS OF A LAUNCHER STRUCTURE IN «ROCKET STRUCTURE – PROPULSION SYSTEM» DYNAMIC SYSTEM

ÂÇÀªÌÎÄ²ß ÊÀ²ÒÀÖ²ÉÍÈÕ ÊÎËÈÂÀÍÜ Ó Ð²ÄÈÍÍ²É ÐÀÊÅÒÍ²É ÄÂÈÃÓÍÍ²É ÓÑÒÀÍÎÂÖ² ² ÏÎÇÄÎÂÆÍ²Õ ÊÎËÈÂÀÍÜ ÊÎÐÏÓÑÓ ÐÀÊÅÒÈ-ÍÎѲß

ÂÇÀÈÌÎÄÅÉÑÒÂÈÅ ÊÀÂÈÒÀÖÈÎÍÍÛÕ ÊÎËÅÁÀÍÈÉ Â ÆÈÄÊÎÑÒÍÎÉ ÐÀÊÅÒÍÎÉ ÄÂÈÃÀÒÅËÜÍÎÉ ÓÑÒÀÍÎÂÊÅ È ÏÐÎÄÎËÜÍÛÕ ÊÎËÅÁÀÍÈÉ ÊÎÐÏÓÑÀ ÐÀÊÅÒÛ-ÍÎÑÈÒÅËß

43–47
(
5)

Êàðà÷óí Â.Â.,
Ìåëüíèê Â.Í.,
Øèáåöêèé Â.Þ.

INTERACTION OF CONVEX SHELL WITH A STRONG SHOCK WAVE

ÂÇÀªÌÎÄ²ß ÎÏÓÊËί ÎÁÎËÎÍÊÈ Ç ÏÎÒÓÆÍÎÞ ÓÄÀÐÍÎÞ ÕÂÈËÅÞ

ÂÇÀÈÌÎÄÅÉÑÒÂÈÅ ÂÛÏÓÊËÎÉ ÎÁÎËÎ×ÊÈ Ñ ÑÈËÜÍÎÉ ÓÄÀÐÍÎÉ ÂÎËÍÎÉ

48–52
(
5)

Øóëüæåíêî Í.Ã.,
Ãîíòàðîâñêèé Ï.Ï.

REACTION OF SHELL ELEMENTS OF SPACE VEHICLES ON THE IMPULSE ACTION

ÐÅÀÊÖ²ß ÎÁÎËÎÍÊÎÂÈÕ ÅËÅÌÅÍҲ ÊÎÑ̲×ÍÈÕ ÀÏÀÐÀҲ ÍÀ ²ÌÏÓËÜÑÍÅ ÇÁÓÄÆÅÍÍß

ÐÅÀÊÖÈß ÎÁÎËÎ×Å×ÍÛÕ ÝËÅÌÅÍÒΠÊÎÑÌÈ×ÅÑÊÈÕ ÀÏÏÀÐÀÒΠÍÀ ÈÌÏÓËÜÑÍÎÅ ÂÎÇÄÅÉÑÒÂÈÅ

53–58
(
6)

Äâèãàòåëè è ýíåðãîóñòàíîâêè àýðîêîñìè÷åñêèõ ëåòàòåëüíûõ àïïàðàòîâ

Êîíîõ Â.È.,
Êàëèíè÷åíêî È.È.,
Ãîðäèåö È.Í.,
Êóêñà È.Þ.,
Øïàê À.Â.

CREATION OF HYDRAULIC POWER SYSTEM WITH A PNEUMATIC PISTON ACTUATOR FOR THRUST VECTOR CONTROL SYSTEMS

ÑÒÂÎÐÅÍÍß ÄÆÅÐÅË Ã²ÄÐÀÂ˲×Íί ÏÎÒÓÆÍÎÑÒ² Ç ÏÎÐØÍÅÂÈÌ ÏÍÅÂÌÀÒÈ×ÍÈÌ ÏÐÈÂÎÄÎÌ ÄËß ÑÈÑÒÅÌ ÊÅÐÓÂÀÍÍß ÂÅÊÒÎÐÎÌ ÒßÃÈ ÐÀÊÅÒÈ-ÍÎѲß

ÑÎÇÄÀÍÈÅ ÈÑÒÎ×ÍÈÊΠÃÈÄÐÀÂËÈ×ÅÑÊÎÉ ÌÎÙÍÎÑÒÈ Ñ ÏÎÐØÍÅÂÛÌ ÏÍÅÂÌÀÒÈ×ÅÑÊÈÌ ÏÐÈÂÎÄÎÌ ÄËß ÑÈÑÒÅÌ ÓÏÐÀÂËÅÍÈß ÂÅÊÒÎÐÎÌ ÒßÃÈ ÐÀÊÅÒÛ-ÍÎÑÈÒÅËß

59–66
(
8)

Êîâàëåíêî À.Í.,
Áëèøóí Þ.Â.

METHODOLOGICAL FEATURES OF PREPARATION AND TESTING THE OPERABILITY OF HIGH-ALTITUDE LRE WITH FREE GAS INJECTION BLOWDOWN PROPULSION

ÌÅÒÎÄÈ×Ͳ ÎÑÎÁËÈÂÎÑÒ² ϲÄÃÎÒÎÂÊÈ ÒÀ ÏÐÎÂÅÄÅÍÍß ÂÈÏÐÎÁÓÂÀÍÜ Ç ÏÅÐŲÐÊÈ ÏÐÀÖÅÇÄÀÒÍÎÑÒ² ÂÈÑÎÒÍÈÕ ÐÐÄ Ç ÂÈÒÈÑÊÍÎÞ ÑÈÑÒÅÌÎÞ ÏÎÄÀײ ÏÀËÈÂÀ ÇI ÂÄÓÂÎÌ Â²ËÜÍÎÃÎ ÃÀÇÓ

ÌÅÒÎÄÈ×ÅÑÊÈÅ ÎÑÎÁÅÍÍÎÑÒÈ ÏÎÄÃÎÒÎÂÊÈ È ÏÐÎÂÅÄÅÍÈß ÈÑÏÛÒÀÍÈÉ ÏÎ ÏÐÎÂÅÐÊÅ ÐÀÁÎÒÎÑÏÎÑÎÁÍÎÑÒÈ ÂÛÑÎÒÍÛÕ ÆÐÄ Ñ ÂÛÒÅÑÍÈÒÅËÜÍÎÉ ÑÈÑÒÅÌÎÉ ÏÎÄÀ×È ÒÎÏËÈÂÀ ÏÐÈ ÂÄÓÂÅ ÑÂÎÁÎÄÍÎÃÎ ÃÀÇÀ

67–71
(
5)

Âîñêîáîéíèê Ä.Â.,
Ãðóøåíêî À.Ì.

ANALYSIS OF THE ENERGY ANALYSIS OF ENERGY PERFORMANCE FUEL MIXTURE «LIQUID OXYGEN AND ALCOHOL-AMMONIA SOLUTION» IN SELF-PRESSURISED FEED SYSTEM LPRE LOW TRUST

ÀÍÀË²Ç ÅÍÅÐÃÅÒÈ×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÏÀËÈÂÍί ÏÀÐÈ «Ð²ÄÊÈÉ ÊÈÑÅÍÜ ² ÑÏÈÐÒÎ-À̲À×ÍÈÉ ÐÎÇ×ÈÍ»  ÑÀÌÎÂÈÒÈÑÊÍÈÕ ÑÈÑÒÅÌÀÕ ÏÎÑÒÀ×ÀÍÍß ÐÐÄÌÒ

ÀÍÀËÈÇ ÝÍÅÐÃÅÒÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÒÎÏËÈÂÍÎÉ ÏÀÐÛ «ÆÈÄÊÈÉ ÊÈÑËÎÐÎÄ È ÑÏÈÐÒÎ-ÀÌÌÈÀ×ÍÛÉ ÐÀÑÒÂÎл  ÑÀÌÎÂÛÒÅÑÍÈÒÅËÜÍÛÕ ÑÈÑÒÅÌÀÕ ÏÎÄÀ×È ÆÐÄÌÒ

72–75
(
4)

Êðèâñóí Ð.Þ.,
Áåñêðîâíûé È.Á.,
Êîðîëåâ Â.Ã.

DESIGN IMPROVEMENT FOR SPECIAL EQUIPMENT OF SOLID ROCKET MOTOR TEST

ÓÄÎÑÊÎÍÀËÅÍÍß ÊÎÍÑÒÐÓÊÖ²¯ ÑÏÅÖ²ÀËÜÍÎÃÎ ÎÁËÀÄÍÀÍÍß ÄËß ÂÈÏÐÎÁÓÂÀÍÍß ÐÄÒÏ

 

ÓÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈÅ ÊÎÍÑÒÐÓÊÖÈÈ ÑÏÅÖÈÀËÜÍÎÃÎ ÎÁÎÐÓÄÎÂÀÍÈß ÄËß ÈÑÏÛÒÀÍÈÉ ÐÄÒÒ

76–79
(
4)

Ðûæêîâ Ñ.Ñ.,
Ðàä÷åíêî À.Í.,
Ôîðäóé Ñ.Ã.

APPROACHES OF ENCREASING EFFICIENCY OF TRIGENERATION PLANTS FOR INTEGRATED ENERGY SUPPLY

ÍÀÏÐßÌÈ Ï²ÄÂÈÙÅÍÍß ÅÔÅÊÒÈÂÍÎÑÒ² ÒÐÈÃÅÍÅÐÀÖ²ÉÍÈÕ ÓÑÒÀÍÎÂÎÊ ÀÂÒÎÍÎÌÍÎÃÎ ÅÍÅÐÃÎÇÀÁÅÇÏÅ×ÅÍÍß

ÍÀÏÐÀÂËÅÍÈß ÏÎÂÛØÅÍÈß ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÒÐÈÃÅÍÅÐÀÖÈÎÍÍÛÕ ÓÑÒÀÍÎÂÎÊ ÀÂÒÎÍÎÌÍÎÃÎ ÝÍÅÐÃÎÎÁÅÑÏÅ×ÅÍÈß

80–85
(
6)

Ðàä÷åíêî Í.È.,
Áîõäàëü Ò.,
Ðàä÷åíêî Ð.Í.,
Êîíîâàëîâ Ä.Â.,
Àíäðååâ À.À.

THREE CONTOUR SCAVENGE AIR COOLING SYSTEM

OF MARINE LOW SPEED DIESEL ENGINE

ÒÐÈÊÎÍÒÓÐÍÀ ÑÈÑÒÅÌÀ ÎÕÎËÎÄÆÅÍÍß ÍÀÄÄÓÂÍÎÃÎ ÏβÒÐß ÑÓÄÍÎÂÎÃÎ ÌÀËÎÎÁÅÐÒÎÂÎÃÎ ÄÈÇÅËß

ÒÐÅÕÊÎÍÒÓÐÍÀß ÒÅÏËÎÈÑÏÎËÜÇÓÞÙÀß ÑÈÑÒÅÌÀ ÎÕËÀÆÄÅÍÈß ÍÀÄÄÓÂÎ×ÍÎÃÎ ÂÎÇÄÓÕÀ ÑÓÄÎÂÎÃÎ ÌÀËÎÎÁÎÐÎÒÍÎÃÎ ÄÈÇÅËß

86–91
(
6)

Áîãóñëàåâ Â.À.,
Äîëìàòîâ À.È.,
Äîëìàòîâ Ä.À.,
Êóêóðóäçà À.Â.,
Õàäæèâàíä Ì.

Electrochemical control of low rate reactions into hexane-oxygen flame

ÅËÅÊÒÐÎղ̲×ÍÅ ÊÅÐÓÂÀÍÍß ÏβËÜÍÈÌÈ ÐÅÀÊÖ²ßÌÈ Ó ÃÅÊÑÀÍÎ-ÊÈÑÍÅÂÎÌÓ ÏÎËÓÌ’¯

ÝËÅÊÒÐÎÕÈÌÈ×ÅÑÊÎÅ ÓÏÐÀÂËÅÍÈÅ ÌÅÄËÅÍÍÛÌÈ ÐÅÀÊÖÈßÌÈ Â ÃÅÊÑÀÍÎ-ÊÈÑËÎÐÎÄÍÎÌ ÏËÀÌÅÍÈ

92–96
(
5)

Ìèõàëêèí À.À.

THE FAN BLADES OF PERSPECTIVE TURBOJETS

Ðîáî÷³ËÎÏÀÒʲ ÂÅÍÒÈËßÒÎÐÀ ÏÅÐÑÏÅÊÒÈÂÍÈÕ ÒÐÄÄ

ÐÀÁÎ×ÈÅ ËÎÏÀÒÊÈ ÂÅÍÒÈËßÒÎÐÀ ÏÅÐÑÏÅÊÒÈÂÍÛÕ ÒÐÄÄ

97–100
(
4)

Ñàëüíèêîâ À.Â.

GAS-TURBINE ENGINE IMPELLER UNIT’S DESIGN-STRESS MULTICRITERION OPTIMIZATION

ÊÎÍÑÒÐÓÊÒÈÂÍÎ-̲ÖͲÑÍÀ ÁÀÃÀÒÎÊÐÈÒÅвÀËÜÍÀ ÎÏÒÈ̲ÇÀÖ²ß ÂÓÇ˲ ÐÎÁÎ×ÈÕ ÊÎË²Ñ ÂÌÄ

ÊÎÍÑÒÐÓÊÒÈÂÍÎ-ÏÐÎ×ÍÎÑÒÍÀß ÌÍÎÃÎÊÐÈÒÅÐÈÀËÜÍÀß ÎÏÒÈÌÈÇÀÖÈß ÓÇËΠÐÀÁÎ×ÈÕ ÊÎËÅÑ ÃÒÄ

101–109
(
9)

Ïàðîâàé Å.Ô.

GTE Free turbine with slide bearings

²ËÜÍÀ ÒÓÐÁ²ÍÀ ÃÒÄ íà ï³äøèïíèêàõ êîâçàííÿ

ÑÂÎÁÎÄÍÀß ÒÓÐÁÈÍÀ ÃÒÄ ÍÀ ÏÎÄØÈÏÍÈÊÀÕ ÑÊÎËÜÆÅÍÈß

110–114
(
5)

Øàòîõèí Â.Ô.,
Öèììåðìàí Ñ.Ä.

EFFECTS OF TURBOGENERATOR PROTECTION SYSTEM SPEED CAPABILITIES ON THE DEVELOPMENT OF THE ROTOR ROLL OVER THE STATOR

ÂÏËÈ ØÂÈÄÊÎIJ¯ ÑÈÑÒÅÌÈ ÇÀÕÈÑÒÓ ÒÓÐÁÎÀÃÐÅÃÀÒÀ ÍÀ ÐÎÇÂÈÒÎÊ ÎÁÊÀÒÓ ÐÎÒÎÐÀ ÏÎ ÑÒÀÒÎÐÓ

ÂËÈßÍÈÅ ÁÛÑÒÐÎÄÅÉÑÒÂÈß ÑÈÑÒÅÌÛ ÇÀÙÈÒÛ ÒÓÐÁÎÀÃÐÅÃÀÒÀ ÍÀ ÐÀÇÂÈÒÈÅ ÎÁÊÀÒÀ ÐÎÒÎÐÀ ÏÎ ÑÒÀÒÎÐÓ

115–126
(
12)

Íàçèí Â.È.

MATHEMATICAL MODEL DOUBLE ANGULAR CONTACT HYDROSTATIC BEARINGS

ÌÀÒÅÌÀÒÈ×ÍÀ ÌÎÄÅËÜ ÇÄÂΪÍÎÃÎ ÐÀIJÀËÜÍÎ-óïîðíîÎÃΠòÄÐÎÑÒÀÒÈ×ÍÎÃÎ Ï²ÄØÈÏÍÈÊÀ

ÌÀÒÅÌÀÒÈ×ÅÑÊÀß ÌÎÄÅËÜ ÑÄÂÎÅÍÍÎÃÎ ÐÀÄÈÀËÜÍÎ-ÓÏÎÐÍÎÃÎ ÃÈÄÐÎÑÒÀÒÈ×ÅÑÊÎÃÎ ÏÎÄØÈÏÍÈÊÀ

127–133
(
7)

Àíàíüåâ Â.Ì.,
Êàëèíèí Ä.Â.,
Êîæàðèíîâ Å.Â.

IMPROVING METHODS OF TURBOFAN GEARBOX DESIGN

ÓÄÎÑÊÎÍÀËÅÍÍß ÌÅÒÎIJ ÏÐÎÅÊÒÓÂÀÍÍß ÇÓÁ×ÀÑÒÈÕ ÏÅÐÅÄÀ× ÐÅÄÓÊÒÎв ÏÐÈÂÎÄÓ ÂÅÍÒÈËßÒÎÐÀ ÒÐÄÄ

ÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈÅ ÌÅÒÎÄΠÏÐÎÅÊÒÈÐÎÂÀÍÈß ÇÓÁ×ÀÒÛÕ ÏÅÐÅÄÀ× ÐÅÄÓÊÒÎÐΠÏÐÈÂÎÄÀ ÂÅÍÒÈËßÒÎÐÀ ÒÐÄÄ

134–139
(
6)

Êðàâ÷åíêî È.Ô.,
Øåðåìåòüåâ À.Â.,
ßêîâåíêî À.Â.

EVOLUTION METHOD MANAGEMENT TASK ON LIFE AVIATION ENGINE FOR CTF

ÐÎÇÂÈÒÎÊ ÌÅÒÎÄÈÊÈ ÊÅÐÓÂÀÍÍß ÄÎÂÅÄÅÍÍß ÀÂIÀÖIÉÍÈÕ ÄÂÈÃÓÍIÂ ÄËß ÓÁË

ÐÀÇÂÈÒÈÅ ÌÅÒÎÄÈÊÈ ÓÏÐÀÂËÅÍÈß ÄÎÂÎÄÊÎÉ ÄÂÈÃÀÒÅËÅÉ ÄËß ÓÁÑ

140–149
(
10)

Âåëèêàíîâà Í.Ï.,
Âåëèêàíîâ Ï.Ã.,
Êèñåëåâ À.Ñ.

EFFECT OF ATMOSPHERIC CONDITIONS FOR USE DURABILITY OF THE TURBINE DISK GAS TURBINE ENGINES

ÂÏËÈ ÀÒÌÎÑÔÅÐÍÈÕ ÓÌΠÍÀ ÄÎÂÃÎÒÐÈÂÀ˲ÑÒÜ ÄÈÑʲ ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓͲÂ

ÂËÈßÍÈÅ ÀÒÌÎÑÔÅÐÍÛÕ ÓÑËÎÂÈÉ ÝÊÑÏËÓÀÒÀÖÈÈ ÍÀ ÄÎËÃÎÂÅ×ÍÎÑÒÜ ÄÈÑÊΠÒÓÐÁÈÍ ÀÂÈÀÖÈÎÍÍÛÕ ÃÒÄ

150–154
(
5)

Ñìûñëîâ À.Ì.,
Ñìûñëîâà Ì.Ê.,
Äóáèí À.È.

VOLUMETRIC STRESSES OF THE COMPRESSOR’S BLADES OF GTE  INVESTIGATION

ÄÎÑË²ÄÆÅÍÍß ÇÀËÈØÊÎÂÈÕ ÎÁ'ªÌÍÈÕ ÍÀÏÐÓÆÅÍÜ Â ËÎÏÀÒÊÀÕ ÊÎÌÏÐÅÑÎÐÀ ÃÒÄ

ÈÑÑËÅÄÎÂÀÍÈÅ ÎÑÒÀÒÎ×ÍÛÕ ÎÁÚ¨ÌÍÛÕ ÍÀÏÐ߯ÅÍÈÉ Â ËÎÏÀÒÊÀÕ ÊÎÌÏÐÅÑÑÎÐÀ ÃÒÄ

155–158
(
4)

Ãîëóá Â.Ï.

THE METHOD OF THE FATIGUE LIFE-TIME CALCULATION OF STRUCTURAL COMPONENTS UNDER  BIAXIAL COMBINED LOADING

ÌÅÒÎÄ ÐÎÇÐÀÕÓÍÊÓ ÄÎÂÃβ×ÍÎÑÒ² ÅËÅÌÅÍҲ ÊÎÍÑÒÐÓÊÖ²É ÂÍÀÑ˲ÄÎÊ ÂÒÎÌÈ ÇÀ ÓÌΠÄÂβÑÍÎÃÎ ÊÎÌÁ²ÍÎÂÀÍÎÃΠ ÍÀÂÀÍÒÀÆÅÍÍß

ÌÅÒÎÄ ÐÀÑ×ÅÒÀ ÓÑÒÀËÎÑÒÍÎÉ ÄÎËÃÎÂÅ×ÍÎÑÒÈ ÝËÅÌÅÍÒΠÊÎÍÑÒÐÓÊÖÈÉ ÏÐÈ ÄÂÓÕÎÑÍÎÌ ÊÎÌÁÈÍÈÐÎÂÀÍÍÎÌ ÍÀÃÐÓÆÅÍÈÈ

159–165
(
7)

Ñèìáèðñêèé Ä.Ô.,
Áðóíàê À.À.

MODEL ANALYSES OF HOLD IMPACT IN THE CYCLE ON THE MATERIAL RESISTANCE TO THE LOW-CYCLE FATIGUE USING LAWS OF REPEATED-STATIC LOADING

ÌÎÄÅËÜͲ ÄÎÑË²ÄÆÅÍÍß ÂÏËÈÂÓ ÂÈÒÐÈÌÊÈ Â ÖÈÊ˲ ÍÀ ÎϲРÌÀÒÅвÀËÓ ÌÀËÎÖÈÊËÎÂ²É ÂÒÎ̲ Ç ÂÈÊÎÐÈÑÒÀÍÍßÌ ÇÀÊÎÍÎ̲ÐÍÎÑÒÅÉ ÏÎÂÒÎÐÍÎ-ÑÒÀÒÈ×ÍÎÃÎ ÍÀÂÀÍÒÀÆÅÍÍß

ÌÎÄÅËÜÍÛÅ ÈÑÑËÅÄÎÂÀÍÈß ÂËÈßÍÈß ÂÛÄÅÐÆÅÊ Â ÖÈÊËÅ ÍÀ ÑÎÏÐÎÒÈÂËÅÍÈÅ ÌÀÒÅÐÈÀËÀ ÌÀËÎÖÈÊËÎÂÎÉ ÓÑÒÀËÎÑÒÈ Ñ  ÈÑÏÎËÜÇÎÂÀÍÈÅÌ ÇÀÊÎÍÎÌÅÐÍÎÑÒÅÉ ÏÎÂÒÎÐÍÎ-ÑÒÀÒÈ×ÅÑÊÎÃÎ ÍÀÃÐÓÆÅÍÈß

166–172
(
7)

Åïèôàíîâ Ñ.Â.,
Ðèíã Í.À.,
Ãëèêñîí È.Ë.,
Øàíüêèí Ñ.È.

RAIN” METHOD MODERNIZING FOR TURBINE ENGINE BASIC COMPONENTS LIFE TIME MONITORING

ÌÎÄÅÐͲÇÀÖ²ß ÌÅÒÎÄÓ «ÄÎÙÓ» ÄËß ÌÎͲÒÎÐÈÍÃÓ ÂÈÐÎÁ²ÒÊÓ ÐÅÑÓÐÑÓ ÎÑÍÎÂÍÈÕ ÄÅÒÀËÅÉ ÃÒÄ

ÌÎÄÅÐÍÈÇÀÖÈß ÌÅÒÎÄÀ «ÄÎÆÄß» ÄËß ÌÎÍÈÒÎÐÈÍÃÀ ÂÛÐÀÁÎÒÊÈ ÐÅÑÓÐÑÀ ÎÑÍÎÂÍÛÕ ÄÅÒÀËÅÉ ÃÒÄ

173–176
(
4)

Ïûëåâ Â.À.,
Áåëîãóá À.Â.,
Îáîäåö Ä.Ê.

PREDICTING THE RESOURCE STRENGTH OF PISTON SMALL-ENGINE AIRCRAFT ENGINES

ÏÐÎÃÍÎÇÓÂÀÍÍß ÐÅÑÓÐÑÍί ̲ÖÍÎÑÒ² ÏÎÐØÍß ËÅÃÊÎÌÎÒÎÐÍÎÃÎ À²ÀÖ²ÉÍÎÃÎ ÄÂÈÃÓÍÀ

ÏÐÎÃÍÎÇÈÐÎÂÀÍÈÅ ÐÅÑÓÐÑÍÎÉ ÏÐÎ×ÍÎÑÒÈ ÏÎÐØÍß ËÅÃÊÎÌÎÒÎÐÍÎÃÎ ÀÂÈÀÖÈÎÍÍÎÃÎ ÄÂÈÃÀÒÅËß

177–182
(
6)

Áèáëèê È.Â.

RELIABILITY ASSESSMENT OF PERFORMANCE BASED ON PROBABILISTIC SUMMATION OF FATIGUE DAMAGES

ÎÖ²ÍÊÀ ÏÎÊÀÇÍÈʲ ÍÀIJÉÍÎÑÒ² ÍÀ ÎÑÍβ ²ÌβÐͲÑÍÎÃΠϲÄÑÓÌÎÂÓÂÀÍÍß ÂÒÎÌÍÈÕ ÏÎØÊÎÄÆÅÍÜ

ÎÖÅÍÊÀ ÏÎÊÀÇÀÒÅËÅÉ ÍÀÄÅÆÍÎÑÒÈ ÍÀ ÎÑÍÎÂÅ ÂÅÐÎßÒÍÎÑÒÍÎÃÎ ÑÓÌÌÈÐÎÂÀÍÈß ÓÑÒÀËÎÑÒÍÛÕ ÏÎÂÐÅÆÄÅÍÈÉ

183–187
(
5)

Óìàíñêèé À.Ï.,
Òåðåíòüåâ À.Å.,
Ñòîðîæåíêî Ì.Ñ.,
Êèñåëü Â.Ì.,
Åâäîêèìåíêî Þ.È.,
Âàð÷åíêî Â.Ò.

EFFECT OF TITANIUM DIBORIDE ADDITIVES ON THE STRUCTURE AND PROPERTIES OF  HVAF-COATINGS OF (Ni-Cr-Si-B) – TiB2 SYSTEM

ÂÏËÈ ÄÈÑÏÅÐÑÍÈÕ ÄÎ̲ØÎÊ ÄÈÁÎÐÈÄÓ ÒÈÒÀÍÓ ÍÀ ÑÒÐÓÊÒÓÐÓ ² ÂËÀÑÒÈÂÎÑÒ² HVAF - ÏÎÊÐÈÒҲ ÑÈÑÒÅÌÈ (Ni-Cr-Si-B) – TiB2

ÂËÈßÍÈÅ ÄÈÑÏÅÐÑÍÛÕ ÄÎÁÀÂÎÊ ÄÈÁÎÐÈÄÀ ÒÈÒÀÍÀ ÍÀ ÑÒÐÓÊÒÓÐÓ È ÑÂÎÉÑÒÂÀ HVAF-ÏÎÊÐÛÒÈÉ ÑÈÑÒÅÌÛ (Ni-Cr-Si-B) – TiB2

188–194
(7)

Ñíåæíîé Ã.Â.

magnetometric EVALUATION OF CORROSION RESISTANCE austenitic chromium-nickel steels with different phase composition

Ìàãí³òîìåòðè÷íà îö³íêà êîðîç³éíî¿ òðèâêîñò³ àóñòåí³òíèõ õðîìîí³êåëåâèõ ÑÒÀËÅÉ â çàëåæíîñò³ â³ä ôàçîâîãî ñêëàäó

ÌÀÃÍÈÒÎÌÅÒÐÈ×ÅÑÊÀß ÎÖÅÍÊÀ ÊÎÐÐÎÇÈÎÍÍÎÉ ÑÒÎÉÊÎÑÒÈ ÀÓÑÒÅÍÈÒÍÛÕ ÕÐÎÌÎÍÈÊÅËÅÂÛÕ ÑÒÀËÅÉ Â ÇÀÂÈÑÈÌÎÑÒÈ ÎÒ ÔÀÇÎÂÎÃÎ ÑÎÑÒÀÂÀ

195–201
(
7)

Âàêóëåíêî Ê.Â.,
Êàçàê È.Á.,
Ñåâèäîâà Å.Ê.

CORROSION RESISTANCE OF STEEL 20X13 With vacuum-plasma coatings

Êîðîç³éíà ñò³éê³ñòü ñòàë³ 20Õ13 ç âàêóóìíî-ïëàçìîâèìè ïîêðèòòÿìè

ÊÎÐÐÎÇÈÎÍÍÀß ÑÒÎÉÊÎÑÒÜ ÑÒÀËÈ 20Õ13 Ñ ÂÀÊÓÓÌÍÎ-ÏËÀÇÌÅÍÍÛÌÈ ÏÎÊÐÛÒÈßÌÈ

202–207
(
6)

Êàèðîâ À.Ñ.,
Ìîðãóí Ñ.À.

TURBINE ENGINES BLADED DISKS SUBMITED AS NON-CYCLICAL SYSTEM VIBRATION, STRESS AND DEFORMATION ANALYSIS

ÊÎËÈÂÀÍÍß ÒÀ ÍÀÏÐÓÆÅÍÎ-ÄÅÔÎÐ̲ÂÍÈÉ ÑÒÀÍ Â²Íֲ ÐÎÁÎ×ÈÕ ËÎÏÀÒÎÊ ÒÓÐÁÎÌÀØÈÍ ÏÐÈ ÏÎÐÓØÅÍͲ ÖÈÊ˲×Íί ÑÈÌÌÅÒв¯

ÊÎËÅÁÀÍÈß È ÍÀÏÐ߯ÅÍÍÎ-ÄÅÔÎÐÌÈÐÎÂÀÍÍÎÅ ÑÎÑÒÎßÍÈÅ ÂÅÍÖΠÐÀÁÎ×ÈÕ ËÎÏÀÒÎÊ ÒÓÐÁÎÌÀØÈÍ ÏÐÈ ÍÀÐÓØÅÍÈÈ ÖÈÊËÈ×ÅÑÊÎÉ ÑÈÌÌÅÒÐÈÈ

208–215
(
8)

Íàçàðåíêî Þ.Á.,
Ïîòàïîâ À.Þ.

NEW APPROACH OF FLOATING INTERSHAFT BEARING SLIPPING ELIMINATION

ÍÎÂÈÉ ÏIÄÕIÄ ÄÎ ÂÈÐIØÅÍÍß ÏÐÎÁËÅÌÈ ÓÑÓÍÅÍÍß ÏÐÎÊÎÂÇÓÂÀÍÍß ÌÀËÎÍÀÂÀÍÒÀÆÅÍÈÕ ÌIÆÂÀËÜÍÛÕ ÏIÄØÈÏÍÈÊIÂ

ÍÎÂÛÉ ÏÎÄÕÎÄ Ê ÐÅØÅÍÈÞ ÏÐÎÁËÅÌÛ ÓÑÒÐÀÍÅÍÈß ÏÐÎÑÊÀËÜÇÛÂÀÍÈß ÑËÀÁÎÍÀÃÐÓÆÅÍÍÛÕ ÌÅÆÂÀËÜÍÛÕ ÏÎÄØÈÏÍÈÊÎÂ

216–219
(
4)

Ìåäâåäîâñêàÿ Ò.Ô.,
Ðæåâñêàÿ È.Å.,
Ìåäâåäåâà Å.Ë.,
Åôèìåíêî Â.Í.,
Çåëåíñêàÿ Î.Í.

STRENGTH OF THE COVER AND POWER PIN GIDROAGREGAT

̲ÖͲÑÒÜ ÊÐÈØÊÈ ² ÑÈËÎÂί ØÏÈËÜÊÈ Ã²ÄÐÎÀÃÐÅÃÀÒÓ ÃÀÅÑ

ÏÐÎ×ÍÎÑÒÜ ÊÐÛØÊÈ È ÑÈËÎÂÎÉ ØÏÈËÜÊÈ ÃÈÄÐÎÀÃÐÅÃÀÒÀ ÃÀÝÑ

220–225
(
6)

Ïàí³í Â.Â.,
Äèêèé Ì.Î.,
Ñîëîìàõà À.Ñ.,
Ïåòðåíêî Â.Ã.

FOG COMPRESSION IN GAS TURBINE ENGINES

ÐÅÀ˲ÇÀÖ²ß «ÂÎËÎÃÎÃÎ ÑÒÈÑÍÅÍÍß»  ÃÀÇÎÒÓÐÁ²ÍÍÈÕ ÄÂÈÃÓÍÀÕ

ÐÅÀËÈÇÀÖÈß «ÂËÀÆÍÎÃÎ ÑÆÀÒÈß» Â ÃÀÇÎÒÓÐÁÈÍÍÛÕ ÄÂÈÃÀÒÅËßÕ

226–230
(
5)

Ãðèãîðüåâ Â.Â.,
Åëàíñêèé À.Â.,
Ïîïóãà À.È.

CONCEPTUAL SCHEMES OF AIRCRAFT ENGINES WITH HIGH FUEL EFFICIENCY

Ïåðñïåêòèâí³ ñõåìè àâ³àö³éíèõ äâèãóí³â ç âèñîêîþ ïàëèâíîþ åôåêòèâí³ñòþ

ÏÅÐÑÏÅÊÒÈÂÍÛÅ ÑÕÅÌÛ ÀÂÈÀÖÈÎÍÍÛÕ ÄÂÈÃÀÒÅËÅÉ Ñ ÂÛÑÎÊÎÉ ÒÎÏËÈÂÍÎÉ ÝÔÔÅÊÒÈÂÍÎÑÒÜÞ

231–236
(
6)

Èíôîðìàöèîííûå òåõíîëîãèè

Äàíèëêèí Ñ.Þ.,
Ðåäüêèí Ä.À.,
Õîðèêîâ À.À.,
Øàíüêèí Ñ.È.

NON-CONTACT DIAGNOSTIC OF THE TURBOMACHINERY ROTOR BLADES RESONANT OSCILLATIONS

ÁÅÇÊÎÍÒÀÊÒÍÀ IJÀÃÍÎÑÒÈÊÀ ÐÅÇÎÍÀÍÑÍÈÕ ÊÎËÈÂÀÍÜ ÐÎÁÎ×ÈÕ ËÎÏÀÒÎÊ ÒÓÐÁÎÌÀØÈÍ

ÁÅÑÊÎÍÒÀÊÒÍÀß ÄÈÀÃÍÎÑÒÈÊÀ ÐÅÇÎÍÀÍÑÍÛÕ ÊÎËÅÁÀÍÈÉ  ÐÀÁÎ×ÈÕ ËÎÏÀÒÎÊ ÒÓÐÁÎÌÀØÈÍ

237–241
(
5)

Òêà÷ Ì.Ð.,
Äîâãàíü Ä.Â.,
Çîëîòîé Þ.Ã.,
Æóê È.Þ.

AUTOMATION OF OSCILLATION FORMS DETERMINATION OF LOW POWER GTE ELEMENTS

ÀÂÒÎÌÀÒÈÇÀÖ²ß ÂÈÇÍÀ×ÅÍÍß ÂËÀÑÍÈÕ ×ÀÑÒÎÒ ² ÔÎÐÌ ÊÎËÈÂÀÍÜ ÅËÅÌÅÍҲ ÒÓÐÁ²Í ÌÀËί ÏÎÒÓÆÍÎÑÒ²

ÀÂÒÎÌÀÒÈÇÀÖÈß ÎÏÐÅÄÅËÅÍÈß ÑÎÁÑÒÂÅÍÍÛÕ ×ÀÑÒÎÒ È ÔÎÐÌ ÊÎËÅÁÀÍÈÉ ÝËÅÌÅÍÒΠÒÓÐÁÈÍ ÌÀËÎÉ ÌÎÙÍÎÑÒÈ

242–248
(
7)

Îãèåíêî Ñ.A.

MICROWAVE RANGE RADIATION OF STATIONARY PLASMA THRUSTER AS RESULT OF TRANSFORMATION OF WAVES IN DISCHARGE INTERVAL PLASMA

ÑÂ× ÂÈÏÐÎ̲ÍÞÂÀÍÍß ÑÒÀÖ²ÎÍÀÐÍÎÃÎ ÏËÀÇÌÎÂÎÃÎ ÄÂÈÃÓÍÀ ßÊ ÍÀÑ˲ÄÎÊ ÒÐÀÍÑÔÎÐÌÀÖ²¯ ÕÂÈËÜ Ó ÏËÀÇ̲ ÐÎÇÐßÄÍÎÃÎ ÏÐÎ̲ÆÊÀ

ÑÂ× ÈÇËÓ×ÅÍÈÅ ÑÒÀÖÈÎÍÀÐÍÎÃÎ ÏËÀÇÌÅÍÍÎÃÎ ÄÂÈÃÀÒÅËß ÊÀÊ ÐÅÇÓËÜÒÀÒ ÒÐÀÍÑÔÎÐÌÀÖÈÈ ÂÎËÍ Â ÏËÀÇÌÅ ÐÀÇÐßÄÍÎÃÎ ÏÐÎÌÅÆÓÒÊÀ

249–253
(
5)

Ìàêñèìåíêî Ò.À.,
Ëîÿí À.Â.,
Ðûáàëîâ Î.Ï.

INVESTIGATIONS OF INTEGRAL CHARACTERISTICS OF SMALL SPT WITH DISCHARGE CHAMBER MADE OF BN COMPOSITIONS

ÄÎÑË²ÄÆÅÍÍß ²ÍÒÅÃÐÀËÜÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÌÀËÎÃÎ ÑÏÄ Ç ÐÎÇÐßÄÍÎÞ ÊÀÌÅÐÎÞ Ç ÁÎÐÎͲÒÐÈÄÍÈÕ ÊÎÌÏÎÇÈÖ²É

ÈÑÑËÅÄÎÂÀÍÈÅ ÈÍÒÅÃÐÀËÜÍÛÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÌÀËÎÃÎ ÑÏÄ Ñ ÐÀÇÐßÄÍÎÉ ÊÀÌÅÐÎÉ ÈÇ ÁÎÐÎÍÈÒÐÈÄÍÛÕ ÊÎÌÏÎÇÈÖÈÉ

254–257
(
4)

Öàãëîâ À.È.,
Ëîÿí À.Â.,
Ñîëîíèíêî E.Ï.

REDUCTION OF TEST SAMPLE SURFACE TEMPERATURE NONUNIFORMITY DURING ELECTRIC PROPULSION CATHODE’S EMITTERS TESTING

̲Ͳ̲ÇÀÖ²ß ÒÅÌÏÅÐÀÒÓÐÍί ÍÅвÂÍÎ̲ÐÍÎÑÒ² ÏÎÂÅÐÕͲ ÄÎÑË²ÄÆÓÂÀÍÎÃÎ ÇÐÀÇÊÀ ÏÐÈ ÂÈÏÐÎÁÓÂÀÍÍßÕ Å̲ÒÅв ÊÀÒÎIJ ÅÐÄ

ÌÈÍÈÌÈÇÀÖÈß ÒÅÌÏÅÐÀÒÓÐÍÎÉ ÍÅÐÀÂÍÎÌÅÐÍÎÑÒÈ ÏÎÂÅÐÕÍÎÑÒÈÈÑÑËÅÄÓÅÌÎÃÎ ÎÁÐÀÇÖÀ ÏÐÈ ÈÑÏÛÒÀÍÈßÕ ÝÌÈÒÒÅÐÎÂ ÊÀÒÎÄÎÂ ÝÐÄ

258–261
(
4)

Íåñòåðåíêî Ñ.Þ.,
Ðîøàíïóð Ø.

PECULIARITIES OF ELECTRONS REFLECTION FROM POTENTIAL BARRIER AND THEIR GAS DYNAMICS CHATACTERISTICS FLOWS ON THE BORDERS OF ELECTRIC PROPULSION THTUSTERS PLASMA

ÎÑÎÁËÈÂÎÑÒ² ²ÄÁÈÒÒß ÅËÅÊÒÐÎÍ²Â Â²Ä ÏÎÒÅÍÖ²ÀËÜÍÎÃÎ ÁÀÐ'ªÐÓ ² ÏÎÒÎÊÈ ¯Õ ÃÀÇÎÄÈÍÀ̲×ÍÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÍÀ ÌÅÆÀÕ ÏËÀÇÌÈ ÅËÅÊÒÐÎÐÀÊÅÒÍÈÕ ÄÂÈÃÓͲÂ

ÎÑÎÁÅÍÍÎÑÒÈ ÎÒÐÀÆÅÍÈß ÝËÅÊÒÐÎÍΠÎÒ ÏÎÒÅÍÖÈÀËÜÍÎÃÎ ÁÀÐÜÅÐÀ È ÏÎÒÎÊÈ ÈÕ ÃÀÇÎÄÈÍÀÌÈ×ÅÑÊÈÕ ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÍÀ ÃÐÀÍÈÖÀÕ ÏËÀÇÌÛ ÝËÅÊÒÐÎÐÀÊÅÒÍÛÕ ÄÂÈÃÀÒÅËÅÉ

262–265
(
4)

Áåçðó÷êî Ê.Â.,
Áóðûì È.Ã.,
Äàâèäîâ À.Î.,
Ôðîëîâ Â.Ï.,
Øèðèíñêèé Ñ.Â.

METHOD OF ESTIMATION OF EFFICIENCY OF SPACEPORTS AND THEIR SYSTEMS DURING THE DESIGN PHASE

ÌÅÒÎÄÈÊÀ ÎÖ²ÍÊÈ ÅÔÅÊÒÈÂÍÎÑÒ² ÊÎÑÌÎÄÐÎ̲ ÒÀ ¯Õ ÑÈÑÒÅÌ ÍÀ ÅÒÀϲ ÏÐÎÅÊÒÓÂÀÍÍß

ÌÅÒÎÄÈÊÀ ÎÖÅÍÊÈ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÊÎÑÌÎÄÐÎÌÎÂ È ÈÕ ÑÈÑÒÅÌ ÍÀ ÝÒÀÏÅ ÏÐÎÅÊÒÈÐÎÂÀÍÈß

266–270
(
5)

Äçåíçåðñêèé Â.À.,
Êàçà÷à Þ.È.,
Øíóðîâîé Ñ.Â.,
Áóðûëîâ Ñ.Â.,
Ñêîñàðü Â.Þ.

IMPROVEMENT OF TECHNOLOGIES OF LEAD BATTERY GRID MANUFACTURING

ÓÄÎÑÊÎÍÀËÅÍÍß ÒÅÕÍÎËÎÃ²É ÂÈÃÎÒÎÂËÅÍÍß ÑÒÐÓÌβÄÂÎIJ ÄËß ÑÂÈÍÖÅÂÈÕ ÀÊÓÌÓËßÒÎвÂ

ÓÑÎÂÅÐØÅÍÑÒÂÎÂÀÍÈÅ ÒÅÕÍÎËÎÃÈÉ ÈÇÃÎÒÎÂËÅÍÈß ÒÎÊÎÎÒÂÎÄÎÂ ÄËß ÑÂÈÍÖÎÂÛÕ ÀÊÊÓÌÓËßÒÎÐÎÂ

271–275
(
5)

Äàíîâ À.Ñ.

VECTOR NATURE OF COMMON FIELD OF INTERACTION

ÂÅÊÒÎÐÍÀ ÏÐÈÐÎÄÀ ªÄÈÍÎÃÎ ÏÎËß ÂÇÀªÌÎIJ¯

ÂÅÊÒÎÐÍÀß ÏÐÈÐÎÄÀ ÅÄÈÍÎÃÎ ÏÎËß ÂÇÀÈÌÎÄÅÉÑÒÂÈß

276–279
(
4)

Êó÷óê Ã.À.

SYNTHESIS OF DATA DEPOSITORY CLOUD HYBRID TOPOLOGY IN HETEROGENEOUS NETWORK

ÑÈÍÒÅÇ ÒÎÏÎËÎò¯ òÁÐÈÄÍÎÃÎ ÕÌÀÐÍÎÃÎ ÑÕÎÂÈÙÀ ÄÀÍÈÕ Ó ÃÅÒÅÐÎÃÅÍÍÎÌÓ ÑÅÐÅÄÎÂÈÙ²

ÑÈÍÒÅÇ ÒÎÏÎËÎÃÈÈ ÃÈÁÐÈÄÍÎÃÎ ÎÁËÀ×ÍÎÃÎ ÕÐÀÍÈËÈÙÀ ÄÀÍÍÛÕ Â ÃÅÒÅÐÎÃÅÍÍÎÉ ÑÐÅÄÅ

280–284
(
5)

 

 

 

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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. ïîñòàíîâëåíèå ïðåçèäèóìà ÂÀÊ Óêðàèíû ¹1-05/4 îò 14.10.2009 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 íàóêîìåòðè÷åñêèå áàçû äàííûõ: íàó÷íîé ýëåêòðîííîé áèáëèîòåêè eLIBRARY.RU (Ðîññèéñêàÿ Ôåäåðàöèÿ); Index Copernicus (Ïîëüøà); Google Scholar.