RU2014117915A - SPACE DEVICE OF BLOCK-MODULAR EXECUTION - Google Patents
SPACE DEVICE OF BLOCK-MODULAR EXECUTION Download PDFInfo
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- RU2014117915A RU2014117915A RU2014117915/11A RU2014117915A RU2014117915A RU 2014117915 A RU2014117915 A RU 2014117915A RU 2014117915/11 A RU2014117915/11 A RU 2014117915/11A RU 2014117915 A RU2014117915 A RU 2014117915A RU 2014117915 A RU2014117915 A RU 2014117915A
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- RU
- Russia
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- mpn
- spacecraft
- payload
- modules
- block
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- Monitoring And Testing Of Transmission In General (AREA)
- Radio Relay Systems (AREA)
Abstract
1. Космический аппарат блочно-модульного исполнения, содержащий модули космического аппарата (КА), интерфейсы для обеспечения питанием, интерфейсы для передачи данных и других сигналов, имеющий достаточно места для укладки больших компонентов, отличающийся тем, что в состав КА входят модуль служебных систем, первый модуль полезной нагрузки и второй модуль полезной нагрузки (МПН), причем второй МПН устанавливается на первый МПН так, что стартовая нагрузка второго МПН передается на первый МПН и воспринимается им.2. Космический аппарат по п. 1, отличающийся тем, что космический аппарат может содержать множество модулей полезной нагрузки.3. Космический аппарат по пп. 1 и 2, отличающийся тем, что модули полезной нагрузки могут быть установлены «пакетами».1. A block-modular spacecraft containing modules of the spacecraft (SC), interfaces for supplying power, interfaces for transmitting data and other signals, having enough space for laying large components, characterized in that the SC includes a service system module, the first payload module and the second payload module (MPN), the second MPN being installed on the first MPN so that the starting load of the second MPN is transmitted to the first MPN and is perceived by it. 2. A spacecraft according to claim 1, characterized in that the spacecraft may contain many payload modules. The spacecraft in PP. 1 and 2, characterized in that the payload modules can be installed "packages".
Claims (3)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2014117915/11A RU2581274C2 (en) | 2014-04-29 | 2014-04-29 | Modular spacecraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2014117915/11A RU2581274C2 (en) | 2014-04-29 | 2014-04-29 | Modular spacecraft |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2014117915A true RU2014117915A (en) | 2015-11-10 |
RU2581274C2 RU2581274C2 (en) | 2016-04-20 |
Family
ID=54536242
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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RU2014117915/11A RU2581274C2 (en) | 2014-04-29 | 2014-04-29 | Modular spacecraft |
Country Status (1)
Country | Link |
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RU (1) | RU2581274C2 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2659343C1 (en) * | 2017-02-28 | 2018-06-29 | Акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" | Method of manufacturing of the spacecraft payload module of a block-modular design |
RU2729906C1 (en) * | 2019-12-05 | 2020-08-13 | Акционерное общество «Информационные спутниковые системы» имени академика М.Ф.Решетнёва» | Spacecraft assembly method |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5152482A (en) * | 1990-06-29 | 1992-10-06 | Standard Space Platforms Corp. | Modular mother satellite bus for subsidiary payloads |
EP0849166A1 (en) * | 1996-12-20 | 1998-06-24 | TRW Inc. | Modular spacecraft architecture |
RU2254265C9 (en) * | 2003-05-07 | 2007-04-20 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр им. М.В. Хруничева" | Method of injection of artificial satellites as main and accompanying payloads into geocentric orbit and device for realization of this method |
RU2420431C2 (en) * | 2009-05-05 | 2011-06-10 | Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) | Spacecraft of flexible configuration for extra payload |
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2014
- 2014-04-29 RU RU2014117915/11A patent/RU2581274C2/en active
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Publication number | Publication date |
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RU2581274C2 (en) | 2016-04-20 |
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