RU2016149724A - CONSTRUCTIVE METHOD FOR REDUCING MICRO ACCELERATION - Google Patents

CONSTRUCTIVE METHOD FOR REDUCING MICRO ACCELERATION Download PDF

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Publication number
RU2016149724A
RU2016149724A RU2016149724A RU2016149724A RU2016149724A RU 2016149724 A RU2016149724 A RU 2016149724A RU 2016149724 A RU2016149724 A RU 2016149724A RU 2016149724 A RU2016149724 A RU 2016149724A RU 2016149724 A RU2016149724 A RU 2016149724A
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RU
Russia
Prior art keywords
constructive method
reducing micro
micro acceleration
reducing
spacecraft
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Application number
RU2016149724A
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Russian (ru)
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RU2016149724A3 (en
Inventor
Андрей Валерьевич Седельников
Дарья Павловна Молявко
Ксения Игоревна Потиенко
Original Assignee
федеральное государственное автономное образовательное учреждение высшего образования "Самарский национальный исследовательский университет имени академика С.П. Королёва"
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Application filed by федеральное государственное автономное образовательное учреждение высшего образования "Самарский национальный исследовательский университет имени академика С.П. Королёва" filed Critical федеральное государственное автономное образовательное учреждение высшего образования "Самарский национальный исследовательский университет имени академика С.П. Королёва"
Priority to RU2016149724A priority Critical patent/RU2016149724A/en
Publication of RU2016149724A publication Critical patent/RU2016149724A/en
Publication of RU2016149724A3 publication Critical patent/RU2016149724A3/ru

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Claims (1)

Способ снижения микроускорений, заключающийся в изменении конструкции космического аппарата, отличающийся тем, что с внешней стороны космического аппарата устанавливают стержни, к которым прикреплены грузы, с возможностью перемещения вдоль этих стержней, причем оси стержней проходят через центр масс космического аппарата.A method of reducing microacceleration, which consists in changing the design of the spacecraft, characterized in that on the outside of the spacecraft, rods are mounted to which weights are attached, with the possibility of movement along these rods, the axis of the rods passing through the center of mass of the spacecraft.
RU2016149724A 2016-12-16 2016-12-16 CONSTRUCTIVE METHOD FOR REDUCING MICRO ACCELERATION RU2016149724A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2016149724A RU2016149724A (en) 2016-12-16 2016-12-16 CONSTRUCTIVE METHOD FOR REDUCING MICRO ACCELERATION

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2016149724A RU2016149724A (en) 2016-12-16 2016-12-16 CONSTRUCTIVE METHOD FOR REDUCING MICRO ACCELERATION

Publications (2)

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RU2016149724A true RU2016149724A (en) 2018-06-18
RU2016149724A3 RU2016149724A3 (en) 2018-06-18

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RU2016149724A RU2016149724A (en) 2016-12-16 2016-12-16 CONSTRUCTIVE METHOD FOR REDUCING MICRO ACCELERATION

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RU2016149724A3 (en) 2018-06-18

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Legal Events

Date Code Title Description
FA92 Acknowledgement of application withdrawn (lack of supplementary materials submitted)

Effective date: 20190130