RU2001130535A - Spacecraft solar battery - Google Patents

Spacecraft solar battery

Info

Publication number
RU2001130535A
RU2001130535A RU2001130535/28A RU2001130535A RU2001130535A RU 2001130535 A RU2001130535 A RU 2001130535A RU 2001130535/28 A RU2001130535/28 A RU 2001130535/28A RU 2001130535 A RU2001130535 A RU 2001130535A RU 2001130535 A RU2001130535 A RU 2001130535A
Authority
RU
Russia
Prior art keywords
solar battery
frame
spacecraft
spacecraft solar
additional
Prior art date
Application number
RU2001130535/28A
Other languages
Russian (ru)
Other versions
RU2221731C2 (en
Inventor
Геннадий Георгиевич Кислинский
Виктор Васильевич Билько
Анатолий Петрович Афанасьев
Original Assignee
Государственный научно-производственный ракетно-космический центр "ЦСКБ-Прогресс"
Filing date
Publication date
Application filed by Государственный научно-производственный ракетно-космический центр "ЦСКБ-Прогресс" filed Critical Государственный научно-производственный ракетно-космический центр "ЦСКБ-Прогресс"
Priority to RU2001130535/11A priority Critical patent/RU2221731C2/en
Priority claimed from RU2001130535/11A external-priority patent/RU2221731C2/en
Publication of RU2001130535A publication Critical patent/RU2001130535A/en
Application granted granted Critical
Publication of RU2221731C2 publication Critical patent/RU2221731C2/en

Links

Claims (1)

Солнечная батарея космического аппарата, состоящая из рамы, на которой закреплена основная пирочека, балки, верхних и нижних створок, попарно связанных между собой и установленных на раме жестко, связанной с приводом, закрепленным на корпуса космического аппарата, отличающаяся тем, что на раме установлена дополнительная пирочека, причем штоки основной и дополнительной пирочек взаимодействуют с коромыслом, которое шарнирно связано с кронштейном, жестко закрепленным на нижней створке СБ.The solar battery of the spacecraft, consisting of a frame on which the main pyrocheck, beams, upper and lower shutters are fixed, pairwise interconnected and mounted on the frame rigidly connected to the drive mounted on the spacecraft body, characterized in that the frame is equipped with an additional pyrochek, and the rods of the main and additional pyrochees interact with the beam, which is pivotally connected to an arm rigidly attached to the lower flap of the SB.
RU2001130535/11A 2001-11-12 2001-11-12 Spacecraft solar battery RU2221731C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2001130535/11A RU2221731C2 (en) 2001-11-12 2001-11-12 Spacecraft solar battery

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2001130535/11A RU2221731C2 (en) 2001-11-12 2001-11-12 Spacecraft solar battery

Publications (2)

Publication Number Publication Date
RU2001130535A true RU2001130535A (en) 2003-08-20
RU2221731C2 RU2221731C2 (en) 2004-01-20

Family

ID=32090447

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2001130535/11A RU2221731C2 (en) 2001-11-12 2001-11-12 Spacecraft solar battery

Country Status (1)

Country Link
RU (1) RU2221731C2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2677118C1 (en) * 2017-10-10 2019-01-15 Федеральное государственное унитарное предприятие "Российский Федеральный ядерный центр - Всероссийский научно-исследовательский институт экспериментальной физики" (ФГУП "РФЯЦ-ВНИИЭФ") Node for coupling and uncoupling spaceship structural moving elements
CN109733645B (en) * 2018-12-26 2020-10-27 中国科学院长春光学精密机械与物理研究所 Cabin door connecting assembly

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