MODULAR SPACECRAFT Russian patent published in 2023 - IPC B64G1/10 B64G1/62 

Abstract RU 2801372 C1

FIELD: space technology.

SUBSTANCE: spacecraft (SC) contains a package of sequentially installed one-dimensional cubic modules with service and target equipment. The device is equipped with an aerodynamic braking module. A folded inflatable shell is placed in it. They are connected by means of a flexible hollow halyard. The spacecraft contains a power frame of the lower, three intermediate and the upper horizontal plates, four vertical pins, side panels, a control unit with a timer, a foam generator, batteries and a cover with an electromagnetic lock. Expansion of the shell during its removal from the container into outer space is ensured by the action of the foam entering the shell from the foam generator from the moment the valve and lid are opened at the timer signal until the shell is completely expanded and the foam solidifies.

EFFECT: possibility of reliable and predictable withdrawal of CubeSat-type modular satellites from the working orbit after termination of their regular operation.

2 cl, 4 dwg

Similar patents RU2801372C1

Title Year Author Number
MODULAR SPACECRAFT 2018
  • Mitkin Aleksandr Sergeevich
  • Moskatinev Ivan Vladimirovich
  • Sysoev Valentin Konstantinovich
  • Shirshakov Aleksandr Evgenevich
  • Yudin Andrej Dmitrievich
RU2703818C1
DESCENT TOW VEHICLE FOR RETRIEVING SPACE OBJECTS FROM ORBITS 2015
  • Finchenko Valerij Semenovich
  • Alifanov Oleg Mikhajlovich
  • Kulkov Vladimir Mikhajlovich
  • Firsyuk Sergej Olegovich
  • Terentev Vadim Vasilevich
RU2626788C2
SPACECRAFT WITH AERODYNAMIC BRAKING DEVICE FOR REMOVING SPACE OBJECTS FROM ORBIT INTO EARTH'S ATMOSPHERE AND METHOD FOR CONTROLLING ITS FLIGHT 2020
  • Firsyuk Sergej Olegovich
  • Kulkov Vladimir Mikhajlovich
  • Egorov Yurij Grigorevich
  • Yun Son Uk
RU2748483C1
SCIENTIFIC RESEARCH SPACE APPARATUS RETURNED FROM EARTH ORBIT 2015
  • Finchenko Valerij Semenovich
  • Kulkov Vladimir Mikhajlovich
  • Firsyuk Sergej Olegovich
  • Terentev Vadim Vasilevich
RU2634608C2
DEVICE FOR AERODYNAMIC BRAKING OF SPACECRAFT 2016
  • Leonov Aleksandr Georgievich
  • Efremov Gerbert Aleksandrovich
  • Efremova Olga Mikhajlovna
  • Palkin Maksim Vyacheslavovich
  • Shilo Vladimir Konstantinovich
  • Shiryaev Aleksandr Vladimirovich
RU2671067C2
METHOD FOR ACCELERATING DEORBITAL SPACE VEHICLE THAT COMPLETE ACTIVE FUNCTIONING 2022
  • Poluyan Aleksandr Petrovich
RU2783669C1
METHOD FOR ELIMINATION OF SPACECRAFT LEFT FROM WORKING ORBITS INTO DENSE LAYERS OF ATMOSPHERE, AND DEVICE FOR FRAGMENTATION OF SPACECRAFTS IN DENSE LAYERS OF ATMOSPHERE 2018
  • Afanasev Sergej Mikhajlovich
  • Ankudinov Aleksandr Vladimirovich
RU2708407C1
METHOD FOR LAUNCHING ARTIFICIAL SATELLITES INTO EARTH ORBIT 2018
  • Rossettini, Luca
  • Ferrario, Lorenzo
  • Bevilacqua, Marco
  • Vallini, Lorenzo
RU2770256C2
METHOD OF FORMATION OF A GROUP OF ARTIFICIAL EARTH SATELLITES FOR MONITORING POTENTIALLY DANGEROUS THREATS IN NEAR-EARTH SPACE IN A MODE CLOSE TO REAL TIME 2018
  • Panasyuk Mikhail Igorevich
  • Kovtyukh Aleksandr Semenovich
  • Podzolko Mikhail Vladimirovich
  • Tulupov Vladimir Ivanovich
  • Yashin Ivan Vasilevich
RU2711554C1
METHOD OF WITHDRAWING SPACECRAFT THAT HAS COMPLETED ACTIVE OPERATION FROM GEOSTATIONARY ORBIT 2023
  • Poluyan Aleksandr Petrovich
RU2824862C1

RU 2 801 372 C1

Authors

Shirshakov Aleksandr Evgenevich

Moskatinev Ivan Vladimirovich

Mitkin Aleksandr Sergeevich

Sysoev Valentin Konstantinovich

Yudin Andrej Dmitrievich

Dates

2023-08-08Published

2023-03-31Filed