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2 714 064

(13)

(51)

IPC

B64G1/22(2006-01-01)

B64G1/10(2006-01-01)

B81B7/04(2006-01-01)

(21) (22)

Application

2019111570, 2019-04-16

(24)

Start date

2019-04-16

(22)

Actual filing date

2019-04-16

(45)

Published

2020-02-11

(72)

Inventor

Linkov Vladimir AnatolevichGusev Sergej IgorevichKolesnikov Sergej ValerevichLinkov Yurij VladimirovichLinkov Pavel VladimirovichTaganov Aleksandr Ivanovich

(73)

Holder

Federalnoe Gosudarstvennoe Byudzhetnoe Obrazovatelnoe Uchrezhdenie Vysshego Obrazovaniya Gosudarstvennyj Radiotekhnicheskij Universitet"

BINARY SPACECRAFT WITH A RECONFIGURABLE ANTENNA COMBINED WITH A FLEXIBLE TAPE SOLAR BATTERY DEPLOYED BY MULTI-VECTOR MATRIX ROCKET ENGINES Russian patent published in 2020 - IPC B64G1/22 B64G1/10 B81B7/04

Abstract RU 2714064 C1

FIELD: spacecraft.

SUBSTANCE: invention relates to design and equipment of small-size satellites intended for creation of antenna systems. Binary spacecraft (BSC) comprises two cubic bodies with swivel telescopic rods accommodating multi-vector matrix rocket engines (MMRE) for deployment of a flexible solar battery integrated with a collinear antenna, data and power buses and a position barcode tape. Tape is connected to control equipment through bar code sensors. For MMRE control by length of dilution and orientation of BSC cases there are four laser range finders and four CCD matrices installed on panels of housings. For connection of BSC to each other in different configurations there are four rotary nanostructured contact pads with controlled adhesion (two – on facets of bodies, free from panels).

EFFECT: enabling MMRE to deploy and roll a solar battery with an antenna and form multi-element antenna systems from several BSCs.

1 cl, 7 dwg

Similar patents RU2714064C1

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RU 2 714 064 C1

Authors

Linkov Vladimir Anatolevich

Gusev Sergej Igorevich

Kolesnikov Sergej Valerevich

Linkov Yurij Vladimirovich

Linkov Pavel Vladimirovich

Taganov Aleksandr Ivanovich

Dates

2020-02-11—Published

2019-04-16—Filed