Íàó÷íûå ×òåíèÿ ïàìÿòè Ê.Ý. Öèîëêîâñêîãî - íàó÷íàÿ êîíôåðåíöèÿ â Êàëóãå

Ïðîáëåìû ðàêåòíîé è êîñìè÷åñêîé òåõíèêè. 2019 ãîä

60 ËÅÒ ÈÑÑËÅÄÎÂÀÍÈß ËÓÍÛ ÊÎÑÌÈ×ÅÑÊÈÌÈ ÀÏÏÀÐÀÒÀÌÈ. 60 YEARS OF THE MOON’S EXPLORATION BY SPACECRAFT
À.Â.Ãóñåâ, Õ.Õàíàäà, Æ.Ìåíã, Ç.Ïèíã

ÀÍÀËÈÇ ÂËÈßÍÈß ÏÀÐÀÌÅÒÐΠÄÍÈÙ ÒÎÏËÈÂÍÛÕ ÁÀÊΠÑÂÅÐÕ˨ÃÊÈÕ ÐÀÊÅÒ-ÍÎÑÈÒÅËÅÉ ÍÀ ÌÀÑÑÎÂÛÉ ÊÐÈÒÅÐÈÉ ÝÔÔÅÊÒÈÂÍÎÑÒÈ. ANALYSIS OF THE INFLUENCE OF THE SUPER-SLIGHT LAUNCH VEHICLE FUEL TANKS BOTTOM PARAMETERS ON THE MASS CRITERION OF EFFICIENCY
Ñ.Â.Âèííè÷óê

ÀÍÀËÈÇ ÐÅÇÓËÜÒÀÒÎÂ ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÛÕ ÈÑÑËÅÄÎÂÀÍÈÉ ÃÀÇÎÎÁÐÀÇÍÎÃÎ ÌÅÒÀÍÀ Â ÓÑËÎÂÈßÕ ÅÃÎ ÅÑÒÅÑÒÂÅÍÍÎÉ ÊÎÍÂÅÊÖÈÈ. ANALYSIS OF THE RESULTS OF EXPERIMENTAL STUDIES OF GAS METHANE IN THE CONDITIONS OF ITS NATURAL CONVECTION
Â.À.Àëòóíèí, Ê.Â.Àëòóíèí, Ì.Ð.Àáäóëëèí, Ì.Ë.ßíîâñêàÿ

ÀÍÀËÈÇ ÝÔÔÅÊÒÈÂÍÎÑÒÈ ÏÐÈÌÅÍÅÍÈß ÝËÅÊÒÐÎÑÒÀÒÈ×ÅÑÊÈÕ ÏÎËÅÉ Â ÑÓÙÅÑÒÂÓÞÙÈÕ È ÏÅÐÑÏÅÊÒÈÂÍÛÕ ÑÈÑÒÅÌÀÕ ÑÌÀÇÊÈ ÄÂÈÃÀÒÅËÅÉ ËÅÒÀÒÅËÜÍÛÕ ÀÏÏÀÐÀÒΠÂÎÇÄÓØÍÎÃÎ È ÀÝÐÎÊÎÑÌÈ×ÅÑÊÎÃÎ ÁÀÇÈÐÎÂÀÍÈß. ANALYSIS OF EFFICIENCY OF THE APPLICATION OF ELECTROSTATIC FIELDS IN EXISTING AND PERSPECTIVE LUBRICATION SYSTEMS OF AIRCRAFT ENGINES, AIR AND AEROSPACE BASED
Â.À.Àëòóíèí, Ì.Â.Ëüâîâ, Ä.Â.Êîøåëåâ, À.Ñ.Êàñüêîâ, À.À.Ùèãîëåâ, Ì.Ë.ßíîâñêàÿ

ÈÑÏÎËÜÇÎÂÀÍÈÅ ÌÀÃÍÈÒÍÛÕ ÏÎËÅÉ ÄËß ÇÀÙÈÒÛ ÊÎÑÌÈ×ÅÑÊÈÕ ÊÎÐÀÁËÅÉ ÂÎ ÂÐÅÌß ÌÅÆÏËÀÍÅÒÍÛÕ ÏÎ˨ÒÎÂ. USE OF MAGNETIC FIELDS FOR PROTECTION OF SPACE SHIPS DURING INTERPLANETARY FLIGHTS
À.Ê.Âåäíèêîâ, À.Å.Òàõìàçÿí, Í.È.Çâàðè÷óê

ÈÑÏÎËÜÇÎÂÀÍÈÅ ÒÃÊ «ÏÐÎÃÐÅÑÑ» ÄËß ÏÐÎÂÅÄÅÍÈß ÈÑÑËÅÄÎÂÀÍÈÉ ÊÎÍÂÅÊÒÈÂÍÎÃÎ ÒÅÏËÎÌÀÑÑÎÎÁÌÅÍÀ. USING OF THE “PROGRESS” VEHICLE FOR RESEARCH OF CONVECTIVE HEAT AND MASS TRANSFER
Ä.Ì.Àþêàåâà, Ò.Â.Ìàòâååâà

ÈÑÏÎËÜÇÎÂÀÍÈÅ ÒÅËÅÓÏÐÀÂËÅÍÈß ÏÐÈ ÐÀÁÎÒÅ Ñ ÔÎÒÎ- È ÑÏÅÊÒÐÎÌÅÒÐÈ×ÅÑÊÎÉ ÀÏÏÀÐÀÒÓÐÎÉ ÌÅÆÄÓÍÀÐÎÄÍÎÉ ÊÎÑÌÈ×ÅÑÊÎÉ ÑÒÀÍÖÈÈ. USING TELECONTROL IN WORK WITH PHOTO AND SPECTROMETRIC EQUIPMENT OF THE INTERNATIONAL SPACE STATION
Ì.Þ.Áåëÿåâ, Ä.Þ.Êàðàâàåâ, È.Â.Ðàññêàçîâ

ËÓÍÍÛÉ ÑÊÀÔÀÍÄÐ È ÑÐÅÄÑÒÂÀ ÎÁÅÑÏÅ×ÅÍÈß «ÂÛÕÎÄÀ» ÍÀ ÏÎÂÅÐÕÍÎÑÒÜ ËÓÍÛ. LUNAR SPACESUIT AND MEANS OF PROVIDING «EXIT» ON THE MOON SURFACE
À.À.Àëòóíèí, Í.Ð.Æàìàëåòäèíîâ

ÍÀÓ×ÍÀß ÀÏÏÀÐÀÒÓÐÀ «ÈÊÀÐÓÑ» ÊÎÑÌÈ×ÅÑÊÎÃÎ ÝÊÑÏÅÐÈÌÅÍÒÀ «ÓÐÀÃÀÍ» ÍÀ ÁÎÐÒÓ ÑËÓÆÅÁÍÎÃÎ ÌÎÄÓËß ÐÎÑÑÈÉÑÊÎÃÎ ÑÅÃÌÅÍÒÀ ÌÊÑ. SCIENTIFIC EQUIPMENT "ICARUS" SPACE EXPERIMENT "URAGAN" ON BOARD SERVICE MODULE OF THE RUSSIAN SEGMENT ISS
Ä.Ì.Àþêàåâà, Î.Í.Âîëêîâ

ÍÅÌÅÖÊÀß ÍÀÇÅÌÍÀß ÑÒÀÍÖÈß ÍÎÉØÒÐÅËÈÖ – ÓÇÅË ÍÀÁËÞÄÅÍÈß ÇÅÌËÈ Â ÐÅÆÈÌÅ ÏÑÅÂÄÎÐÅÀËÜÍÎÃÎ ÂÐÅÌÅÍÈ. GERMAN GROUND STATION NEUSTRELITZ – NODE FOR EARTH OBSERVATION NEAR REAL TIME SERVICES
H.Maass, M.Berg, H.Damerow, K.-D.Missling, E.Schwarz

Î ÏÅÐÑÏÅÊÒÈÂÀÕ ÐÅÀËÈÇÀÖÈÈ ÑÏÎÑÎÁÀ ÐÀÇÃÎÍÀ ÊÎÑÌÈ×ÅÑÊÎÃÎ ËÅÒÀÒÅËÜÍÎÃÎ ÀÏÏÀÐÀÒÀ Ñ ÈÑÏÎËÜÇÎÂÀÍÈÅÌ ÊÀÒÀÏÓËÜÒÍÎ ÎÒÁÐÀÑÛÂÀÅÌÎÃÎ ÌÍÎÃÎÐÀÇÎÂÎÃÎ ÐÀÇÃÎÍÍÎÃÎ ÁËÎÊÀ. ON THE PROSPECTS FOR THE IMPLEMENTATION OF THE SPACECRAFT ACCELERATION METHOD USING CATAPULT EJECTED REUSABLE ACCELERATION UNIT
Ñ.Í.Õóäÿêîâ

ÎÏÐÅÄÅËÅÍÈÅ ÎÐÁÈÒÛ ÌÅÆÄÓÍÀÐÎÄÍÎÉ ÊÎÑÌÈ×ÅÑÊÎÉ ÑÒÀÍÖÈÈ ÏÎ ÑÄÅËÀÍÍÛÌ Ñ ÍŨ ÑÍÈÌÊÀÌ ÏÎÂÅÐÕÍÎÑÒÈ ÇÅÌËÈ. DETERMINATION OF THE INTERNATIONAL SPACE STATION ORBIT USING EARTH SURFACE PHOTOS TAKEN FROM THE STATION
Ì.Þ.Áåëÿåâ, Ï.À.Áîðîâèõèí, Ä.Þ.Êàðàâàåâ, Â.Â.Ñàçîíîâ

ÎÒÐÀÁÎÒÊÀ ÌÅÒÎÄΠÎÏÐÅÄÅËÅÍÈß ÕÀÐÀÊÒÅÐÈÑÒÈÊ ÄÂÈÆÅÍÈÉ ÊÎÑÌÎÍÀÂÒΠÌÊÑ Â ÊÎÑÌÈ×ÅÑÊÎÌ ÝÊÑÏÅÐÈÌÅÍÒÅ «ÒÀÉÌÅл. PRACTICING METHODS FOR DETERMINING THE CHARACTERISTICS OF THE MOVEMENTS OF COSMONAUTS OF THE ISS IN THE “TIMER” SPACE EXPERIMENT
Í.À.Òàðàñîâà, È.Â.Ðàññêàçîâ

ÎÖÅÍÊÀ ƨÑÒÊÎÑÒÈ ÊÎÍÑÒÐÓÊÖÈÉ ÊÎÑÌÈ×ÅÑÊÈÕ ÀÏÏÀÐÀÒÎÂ, ÂÛÏÎËÍÅÍÍÛÕ ÈÇ ÊÎÌÏÎÇÈÖÈÎÍÍÛÕ ÌÀÒÅÐÈÀËÎÂ,  ÕÎÄÅ ÏÐȨÌÍÛÕ ÈÑÏÛÒÀÍÈÉ. EVALUATION OF SPACECRAFT COMPOSITE STRUCTURE RIGIDITY DURING INSPECTION TEST
Î.Ã.Äåìåíêî

ÎÖÅÍÊÀ ÏÐÈÐÀÙÅÍÈß ÑÊÎÐÎÑÒÈ ÊÎÑÌÈ×ÅÑÊÎÃÎ ËÅÒÀÒÅËÜÍÎÃÎ ÀÏÏÀÐÀÒÀ ÍÀ ËÀÇÅÐÍÎÉ ÒßÃÅ. EVALUATION OF INCREASE OF SPEED OF SPACECRAFT BY A LASER PROPULSION
À.Ã.Ñàòòàðîâ, À.Â.Ñî÷íåâ, À.Ð.Áèêìó÷åâ, Á.Ð.Çèãàíøèí

ÏÐÎÅÊÒÈÐÎÂÀÍÈÅ ÄÅßÒÅËÜÍÎÑÒÈ ÏÅÐÑÎÍÀËÀ ÏÎ ÎÁÅÑÏÅ×ÅÍÈÞ ÁÅÇÎÏÀÑÍÎÑÒÈ ÑËÎÆÍÎÃÎ ÊÎÌÏËÅÊÑÀ. DESIGNING THE PERSONNEL'S ACTIVITIES TO ENSURE THE SAFETY OF A COMPLEX
Ñ.Â.Áðîííèêîâ

ÏÐÎÅÊÒÈÐÎÂÀÍÈÅ ÐÓ×ÍÛÕ ÔÎÒÎÑÚ¨ÌÎÊ ÍÀ ÏÈËÎÒÈÐÓÅÌÎÌ ÊÎÑÌÈ×ÅÑÊÎÌ ÀÏÏÀÐÀÒÅ. DESIGN OF MANUAL PHOTOS ON THE MANNED SPACECRAFT
Ñ.Â.Áðîííèêîâ, À.Ñ.Ðîæêîâ, Å.È.Ìàëèìåíêîâ, À.Ï.Ãóñåâ

ÐÀÇÐÀÁÎÒÊÀ ÍÎÂÛÕ ÊÎÍÑÒÐÓÊÒÈÂÍÛÕ ÑÕÅÌ ÑÈÑÒÅÌ ÒÅÐÌÎÑÒÀÁÈËÈÇÀÖÈÈ ÎÐÁÈÒÀËÜÍÛÕ ÊÎÑÌÈ×ÅÑÊÈÕ ÑÒÀÍÖÈÉ. DEVELOPMENT OF NEW CONSTRUCTIVE DIAGRAMS OF THERMAL STABILIZATION SYSTEMS OF ORBITAL SPACE STATIONS
Â.À.Àëòóíèí, Ê.Â.Àëòóíèí, Ð.Ð.Êàëèìóëëèí, Ì.Ë.ßíîâñêàÿ

ÐÅÇÓËÜÒÀÒÛ ÝÊÑÏÅÐÈÌÅÍÒÀËÜÍÎÉ ÎÖÅÍÊÈ ÑÊÎÐÎÑÒÈ ÃÐÀÂÈÒÀÖÈÎÍÍÎÃÎ ÂÇÀÈÌÎÄÅÉÑÒÂÈß ÏÐÈ ÑÎËÍÅ×ÍÎÌ ÇÀÒÌÅÍÈÈ È ÏÐÈËÈÂÀÕ. RESULTS OF EXPERIMENTAL ASSESSMENT OF SPEED OF GRAVITATIONAL INTERACTION AT THE SOLAR ECLIPSE AND TIDES
À.È.Ãíåâêî, Ì.Â.Ìóêîìåëà, Ñ.Í.Ñîëîâîâ, Þ.Â.Ðîäèîíîâ, Â.À.ßíóøêåâè÷

ÓÏÐÀÂËÅÍÈÅ ÏÎ˨ÒÎÌ ÊÎÑÌÈ×ÅÑÊÎÃÎ ÊÎÐÀÁËß ÍÀ ÎÑÍÎÂÅ ÑÖÅÍÀÐÍÎÃÎ ÌÎÄÅËÈÐÎÂÀÍÈß. SPACE VEHICLE CONTROL ON THE BASIS OF SCENARIOUS MODELING
À.Â.Äîíñêîâ