FIELD: aerospace engineering.
SUBSTANCE: invention relates to aerospace engineering, particularly, to satellite launch devices. Device for group launching of satellites is made in the form of a column of identical sections connected to each other and made in the form of tetrahedral trusses. Farm of each section comprises four lengthwise posts, top and bottom belts with support assemblies connected with lengthwise posts, transverse power elements and diagonal braces. Braces are made in cross section with profile in form of double tee and are attached to each other near their centers. Section of device are equipped with frames, beams of which are made in cross section in form of U-profile. Outer belt of the frames are made so that to enable attachment of launched satellites, and inner belts are fixed on diagonal braces. Jointing points of frame beams with each other are equipped with support platforms, which are connected to inner beams of beams and are made with possibility of arrangement of frame attachment elements to said diagonal braces on said sites.
EFFECT: device weight reduction is achieved.
5 cl, 5 dwg
             
         
            
              
                | Title | Year | Author | Number | 
							
              
                | DEVICE FOR GROUP LAUNCH OF SATELLITES AND REINFORCED FRAME | 2020 | 
										Ishin Sergej VyacheslavovichFedoskin Dmitrij IgorevichYakovlev Boris DmitrievichVikulenkov Viktor PavlovichZhumakhanov Nursultan BeketzhanovichPoreshnev Anton YurevichChikhanov Evgenij SergeevichBordadymov Viktor EvgenevichSayapin Viktor Ivanovich | RU2725824C1 | 
							
              
                | ADAPTER FOR WAY LOOSE OF USEFUL LOAD | 2016 | 
										Asyushkin Vladimir AndreevichIshin Sergej VyacheslavovichFedoskin Dmitrij IgorevichYakovlev Boris DmitrievichZhumakhanov Nursultan BeketzhanovichOgorodnikov Vadim AleksandrovichZhavoronkov Valerij VladislavovichIlin Sergej AleksandrovichChikhanov Evgenij SergeevichKhoroshenkaya Olga ViktorovnaZakataev Kirill VladimirovichBiryukov Andrej SergeevichBordadymov Viktor EvgenevichSayapin Viktor Ivanovich | RU2624959C1 | 
							
              
                | TRANSFER COMPARTMENT OF CARRIER ROCKET (VERSIONS) | 2015 | 
										Asjushkin Vladimir AndreevichIshin Sergej VjacheslavovichGushchin Viktor GrigorevichOgorodnikov Vadim AleksandrovichBirjukov Andrej SergeevichKalinin Vsevolod IvanovichVikulenkov Viktor PavlovichJakovlev Boris DmitrievichChikhanov Evgenij SergeevichTimofeev Nikolaj GeorgievichZverev Aleksej ValentinovichKhoroshenkaja Olga Viktorovna | RU2603872C1 | 
							
              
                | TRANSITIONAL TRUSS | 2021 | 
										Makarov Vyacheslav PetrovichKovalev Aleksej VitalevichZverev Aleksej ValentinovichChikhanov Evgenij Sergeevich | RU2779010C1 | 
							
              
                | SPACE VEHICLE | 2017 | 
										Chernykh Mikhail NikolaevichMatyushev Dmitrij AndreevichBiryukov Andrej SergeevichKalinin Vsevolod IvanovichBordadymov Viktor EvgenevichZhavoronkov Valerij VladislavovichTimofeev Nikolaj GeorgievichIlin Sergej AleksandrovichMakarov Vyacheslav Petrovich | RU2673447C9 | 
							
              
                | DOUBLE START SYSTEM AND SUPPORT ASSEMBLY | 2018 | 
										Asyushkin Vladimir AndreevichIshin Sergej VyacheslavovichVikulenkov Viktor PavlovichFedoskin Dmitrij IgorevichPoreshnev Anton YurevichYakovlev Boris DmitrievichZhumakhanov Nursultan BeketzhanovichBiryukov Andrej SergeevichMikhajlov Dmitrij NikolaevichGorovtsov Viktor VladimirovichKlimchenkov Vladimir VasilevichZverev Mikhail AlekseevichMerkusheva Irina Anatolevna | RU2694487C1 | 
							
              
                | SPACECRAFT, ITS PAYLOAD MODULE AND SERVICE SYSTEM MODULE | 2016 | 
										Martynov Maksim BorisovichPichkhadze Konstantin MikhajlovichBabyshkin Vladimir EvgenevichMitkin Aleksandr SergeevichBiryukov Andrej SergeevichKovalev Vyacheslav SergeevichMartynov Boris NikolaevichOgorodnikov Vadim AleksandrovichKalinin Vsevolod IvanovichTimofeev Nikolaj Georgievich | RU2617162C1 | 
							
              
                | SERVICE SYSTEM MODULE | 2015 | 
										Martynov Maksim BorisovichPichkhadze Konstantin MikhajlovichBabyshkin Vladimir EvgenevichMitkin Aleksandr SergeevichLomakin Ilya VladimirovichMartynov Boris NikolaevichBiryukov Andrej SergeevichOgorodnikov Vadim Aleksandrovich | RU2621221C1 | 
							
              
                | DEVICE FOR RESTORING THE DESIGN POSITION OF THE OUTER WALL PANEL OF THE ATTIC OF A LARGE-PANEL BUILDING | 2021 | 
										Petukhov Arkadij AleksandrovichMatveev Andrej VadimovichGoncharov Maksim EvgenevichPermyakov Viktor LeonidovichPapin Ivan Vladimirovich | RU2758824C1 | 
							
              
                | ADAPTER FOR GROUP LAUNCHING OF MICRO-SATELLITES | 2004 | 
										Alle A.Ju.Blinov V.N.Bulygin Ju.V.Evropejtsev A.A.Ivanov N.N.Kasatkin G.M.Markelov V.V.Nesterov B.F.Podzorov V.N. | RU2260551C1 |